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| 코소보에서 KFOR소속으로 활약중인 체코군 MI 17 part 2 | |
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코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods 코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods |
| 코소보에서 KFOR소속으로 활약중인 체코군 MI 17 part 2 | |
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코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods 코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods |
| 코소보에서 KFOR소속으로 활약중인 체코군 MI 17 part 2 | |
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코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods 코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods |
| 코소보에서 KFOR소속으로 활약중인 체코군 MI 17 part 2 | |
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코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods 코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods |
| 코소보에서 KFOR소속으로 활약중인 체코군 MI 17 part 2 | |
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코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods 코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods |
| 코소보에서 KFOR소속으로 활약중인 체코군 MI 17 part 2 | |
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코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods 코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods |
| 코소보에서 KFOR소속으로 활약중인 체코군 MI 17 part 2 | |
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코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods 코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods |
| 코소보에서 KFOR소속으로 활약중인 체코군 MI 17 part 2 | |
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코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods 코소보에서 KFOR소속으로 활약중인 체코군 MI 17Mil Mi 17 Also known as the Mi 8MT NATO reporting name Hip H was developed from the basic Mi 8 airframe it was fitted with the larger TV3 117MT engines rotors and transmission developed for the Mi 14 along with fuselage improvements for heavier loads Optional engines for hot and high conditions are the 1545kW 2070 shp Isotov TV3 117VM Recent exports to China and Venezuela for use in high mountains have the new VK 2500 version of the engine with FADEC control The designation Mi 17 is for export the USSR armed forces call it Mi 8MT The Mi 17 can be recognized because it has the tail rotor on the port side instead of the starboard side and dust shields in front of the engine intakes Engine cowls are shorter than on the TV2 powered Mi 8 not extending as far over the cockpit and an opening for bleed valve outlet is present forward of the exhaust Actual model numbers vary by builder engine type and other options As an example the sixteen new Ulan Ude built machines delivered to the Czech air force in 2005 with VM model engines were designated as Mi 171Sh a development of the Mi 8AMTSh Modifications include a new large door on the right side improved Czech built APU Kevlar plates around the cockpit area and engines Eight have a loading ramp in place of the usual clamshell doors and will load a vehicle up to the size of an SUV The Mi 17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia The MI 17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments It can also be very heavily armed with an extensive array or rockets missiles and guns It is often used to air assault infantry forces to attack the point of penetration reinforce units in contact or disrupt counterattacks Additional missions include attack direct air support electronic warfare airborne early warning medevac search and rescue and minelaying The Mi 17 helicopter developed at the Mil Design Bureau from the Mi 8 helicopter is in serial manufactured at the Kazan Helicopter Production Association and Ulan Ude Aviation Plant The designation Mi 17 is for export the Russian armed forces called it Mi 8MT The Mi 17 can be recognized because it has the tail rotor at the starboard side instead of the port side The Mi 17 added a number of improvements to its predecessor including a vibration damper to increase comfort for crew members and passengers The helicopter features a high thrust to weight ratio pair of TVZ 117MT or TVZ 117VM shaft turbine engines with a takeoff power of 1 900 hp The Mi 17 is capable of single engine flight in the event of loss of power by one engine depending on aircraft mission weight because of an engine load sharing system If one engine fails the other engine s output is automatically increased to allow continued flight The Mi 17 is capable of carrying cargoes in the cabin including long cargo with half open or removed doors external loads or passengers 24 people The Mi 17 can carry up to 30 troops and up to 20 wounded it can also be used for in flight unloading of special cargoes The transport version of the MI 17 helicopter is intended to carry cargoes loads in the cargo compartment including long size cargo with partially opened or removed cargo doors external loads or executives up to 24 persons Interior seats are removable for cargo carrying The rear clamshell doors open an internal winch facilitates loading of heavy freight Floor has tiedown rings throughout The aircraft carries a rescue hoist capable to 150 kg External stores are mounted on weapons racks on each side of the fuselage The Mi 17 has six external hardpoints The Mi 17 is provided with missiles bombs small arms and cannons It carries four missile launchers of the B8V20 type with missiles launched with the aid of an on board PUS 31 71 electrical fire control system The BDZ 57KRVM bomb carrier is used for the attachment of bombs up to 500kg Not all vailable munitions are employed at one time mission dictates weapon configuration The helicopter carries four UPK 23 250 gun containers with GSh 23L 23mm guns and pivoted mounts eight units The forward and aft hemispheres are protected by PKT machine guns with independent power supply and remote control circuits The helicopter may be provided with longrange communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode VARIANTS Mi 17 A mid life upgrade of the widely proliferated Mi 8 HIP H medium assault transport helicopter Initially only the export version was known as the Mi 17 The only visible differences between this variant and the older Mi 8s is that the tail rotor is on the portside rather than the starboard side and crew armor plating Mi 17P A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage The Mi 17P Mi 8MTPB `Hip K derivative is provided with long range communication equipment and a radar and it can carry equipment with phased array antennas for suppression of enemy electronic attack and air defence facilities such as airborne radars air defence artillery weapons control radars surveillance and target detection radars and missile radar homing heads The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode Mi 171 17M 17V Also known as Mi 8MTV and a descendent of the HIP H The engines are upgraded to 2x 2 070 shp Klimov TV3 117VMAs to allow greater rates of climb and hover ceilings yet performance characteristics remain virtually unchanged from the baseline Mi 17 General characteristicsCrew Three two pilots and one engineer Capacity 32 passengers or 4 000 kg 8 800 lb on internal external hardpoints Length 18 42 m 60 ft 5 in Rotor diameter 21 352 m 69 ft 10 in Height 4 76 m 15 ft 7 in Disc area 356 m² 3 830 ft² Empty weight 7 100 kg 15 700 lb Loaded weight 11 100 kg 24 470 lb Max takeoff weight 13 000 kg 28 700 lb Powerplant 2× Klimov TV3 117VM turboshafts 1 450 kW 2225 shp each PerformanceMaximum speed 250 km h 156 mph Range 950 km 594 miles Service ceiling 6 000 m 19 690 ft Rate of climb 8 m s ft min Disc loading 31 kg m² 6 lb ft² Power mass 0 26 kW kg 0 16 hp lb Fuel consumption 600 kg h 1 320 lb h Armamentup to 1 500 kg 3 300 lb of disposable stores on six hardpoints including bombs rockets and gunpods |
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http pim ischool washington edu tools htmRelated ToolsA Sampling of PIM Related Products and PrototypesThe following is a sampling of PIM related products and prototypes The list is guaranteed to be incomplete and is only intended to give you an idea of what is out there The collection of PIM related tools is very large and constantly changing We welcome your suggestions on other products and prototypes to include in future versions of this related tools page Last updated 05 30 04 Annotations and note taking Contact management Document manager Email centered General PIM Hypertext authoring tool Life planner Meeting planner Mobile PDA devices Organization of handwritten notes Paper organizer Project centered Reading and Summarization Record everything Search across email e docs and other information forms Semi structured organization of small pieces of information phone numbers errands to run books to read Task management Virtual 3 d Visualization of information relationships Web organizer Annotations and note takingCyberDeskAndrew Wood Anind Dey and Gregory D Abowd http www cc gatech edu fce cyberdesk Golden RetrieverN Liter Enterprisehttp www n liter com My Personal DiaryCAM Development http www camdevelopment com pim my personal diary default htmNet Snippets Net Snippets Ltd http www netsnippets com OneNote2003 Microsoft http www microsoft com office onenote prodinfo overview mspx ProteusThomas Erickson http www outliners com discuss msgReader$648 mode=dayQueries R Links QRL Nipon Charoenkitkarn Jim Tam Mark H Chignell and Gene Golovchinsky http www cs brown edu memex projects htmlSecure Notes OrganizerSecureAction Research LLC http www secureaction com notes XLibrisBill N Schilit Gene Golovchinsky and Morgan N Price http www fxpal com id=xlibrisYawasLaurent Denoue and Laurence Vignollet http www fxpal com people denoue yawas Contact managementACT Interact Commerce Corporationhttp www act comContact Plus Personal 2 7 cContact Plus Corporation http www contactplus com products personal permain htmContactMapBonnie A Nardi Steve Whittaker Ellen Isaacs Mike Creech Jeff Johnson and John Hainsworth http www izix com pro lightweight contactmap phpProphet 2004 Contact managerAvidian Technologies http www avidian com avidian product aspx n=2Time lter Candace L Sidner http delivery acm org 10 1145 580000 572034 p111 balter pdf key1=572034 key2=9273163801 coll=Portal dl=GUIDE CFID=21022367 CFTOKEN=33191323Quick2Do 1 0 2CodeGrid Software http codegrid tripod com Simple DiaryAaron Whiffinhttp www webbedfeetuk com diary Softwrights Reminder ™Softwrights Inc http www softwrights com rmenu htmTaskmasterBellotti Ducheneaut Howard Smith http peach mie utoronto ca people jacek emailresearch CSCW2002 submissions PARC Taskmaster 20position 20paper pdfTaskViewGwizdka http www cas ibm com archives 2002 papers cascon02 htm francais abs gwizdka htmVirtual 3 dData MountainGeorge Robertson Mary Czerwinski Kevin Larson Daniel C Robbins David Thiel and Maarten van Dantzich http research microsoft com ~ggr Visualization of information relationshipsIdea GraphDanny Ayers http www ideagraph net The BrainTheBrain Technologies Corporation http www thebrain com Default htmVVKB Visual Knowledge Builder Dr Frank Shipman Dr Haowei Hsiehhttp www csdl tamu edu VKB Web organizerBackflipBackflip Inchttp www backflip com login ihtmlFeedDemon RSS Reader for Windows Nick Bradbury Bradbury Software LLC http www bradsoft com feeddemon index aspikeepbookmarks com Software Designs Development Corp http www ikeepbookmarks com linkaGoGo linkaGoGo DBA http www linkagogo com MyYahoo Yahoo Inc http my yahoo com Online FileCabinetMike Giles http www furl netPowerbookmarksLi W S Q Vu E Chang D Agrawal Y Hara and H Takano http www teamxweb com doc relatedWork shtml PowerBookmarksPowermarksKaylon Technologies http www kaylon com power htmlSemantic Blogging for Bibliography Management HP Lab http www hpl hp com semweb biblio htmSurfSaver askSam Systems http www surfsaver com WebWatcherT Joachims D Freitag T Mitchell http www 2 cs cmu edu afs cs cmu edu project theo 6 web agent www project home htmlWayback Machine The Internet Archive http www archive org web web php http pim ischool washington edu tools htmRelated ToolsA Sampling of PIM Related Products and PrototypesThe following is a sampling of PIM related products and prototypes The list is guaranteed to be incomplete and is only intended to give you an idea of what is out there The collection of PIM related tools is very large and constantly changing We welcome your suggestions on other products and prototypes to include in future versions of this related tools page Last updated 05 30 04 Annotations and note taking Contact management Document manager Email centered General PIM Hypertext authoring tool Life planner Meeting planner Mobile PDA devices Organization of handwritten notes Paper organizer Project centered Reading and Summarization Record everything Search across email e docs and other information forms Semi structured organization of small pieces of information phone numbers errands to run books to read Task management Virtual 3 d Visualization of information relationships Web organizer Annotations and note takingCyberDeskAndrew Wood Anind Dey and Gregory D Abowd http www cc gatech edu fce cyberdesk Golden RetrieverN Liter Enterprisehttp www n liter com My Personal DiaryCAM Development http www camdevelopment com pim my personal diary default htmNet Snippets Net Snippets Ltd http www netsnippets com OneNote2003 Microsoft http www microsoft com office onenote prodinfo overview mspx ProteusThomas Erickson http www outliners com discuss msgReader$648 mode=dayQueries R Links QRL Nipon Charoenkitkarn Jim Tam Mark H Chignell and Gene Golovchinsky http www cs brown edu memex projects htmlSecure Notes OrganizerSecureAction Research LLC http www secureaction com notes XLibrisBill N Schilit Gene Golovchinsky and Morgan N Price http www fxpal com id=xlibrisYawasLaurent Denoue and Laurence Vignollet http www fxpal com people denoue yawas Contact managementACT Interact Commerce Corporationhttp www act comContact Plus Personal 2 7 cContact Plus Corporation http www contactplus com products personal permain htmContactMapBonnie A Nardi Steve Whittaker Ellen Isaacs Mike Creech Jeff Johnson and John Hainsworth http www izix com pro lightweight contactmap phpProphet 2004 Contact managerAvidian Technologies http www avidian com avidian product aspx n=2Time lter Candace L Sidner http delivery acm org 10 1145 580000 572034 p111 balter pdf key1=572034 key2=9273163801 coll=Portal dl=GUIDE CFID=21022367 CFTOKEN=33191323Quick2Do 1 0 2CodeGrid Software http codegrid tripod com Simple DiaryAaron Whiffinhttp www webbedfeetuk com diary Softwrights Reminder ™Softwrights Inc http www softwrights com rmenu htmTaskmasterBellotti Ducheneaut Howard Smith http peach mie utoronto ca people jacek emailresearch CSCW2002 submissions PARC Taskmaster 20position 20paper pdfTaskViewGwizdka http www cas ibm com archives 2002 papers cascon02 htm francais abs gwizdka htmVirtual 3 dData MountainGeorge Robertson Mary Czerwinski Kevin Larson Daniel C Robbins David Thiel and Maarten van Dantzich http research microsoft com ~ggr Visualization of information relationshipsIdea GraphDanny Ayers http www ideagraph net The BrainTheBrain Technologies Corporation http www thebrain com Default htmVVKB Visual Knowledge Builder Dr Frank Shipman Dr Haowei Hsiehhttp www csdl tamu edu VKB Web organizerBackflipBackflip Inchttp www backflip com login ihtmlFeedDemon RSS Reader for Windows Nick Bradbury Bradbury Software LLC http www bradsoft com feeddemon index aspikeepbookmarks com Software Designs Development Corp http www ikeepbookmarks com linkaGoGo linkaGoGo DBA http www linkagogo com MyYahoo Yahoo Inc http my yahoo com Online FileCabinetMike Giles http www furl netPowerbookmarksLi W S Q Vu E Chang D Agrawal Y Hara and H Takano http www teamxweb com doc relatedWork shtml PowerBookmarksPowermarksKaylon Technologies http www kaylon com power htmlSemantic Blogging for Bibliography Management HP Lab http www hpl hp com semweb biblio htmSurfSaver askSam Systems http www surfsaver com WebWatcherT Joachims D Freitag T Mitchell http www 2 cs cmu edu afs cs cmu edu project theo 6 web agent www project home htmlWayback Machine The Internet Archive http www archive org web web php |
