KVTK (rocket stage)
Manufacturer | Khrunichev State Research and Production Space Center |
---|---|
Country of origin | Template:Russia |
Used on | Angara A5 (proposed upper stage) |
General characteristics | |
Height | 10.4 meters (34 ft)[1] |
Diameter | 3.8 meters (12 ft)[1] |
Gross mass | 23,530 kilograms (51,870 lb)[1] |
Propellant mass | 19,600 kilograms (43,200 lb)[1] |
Engine details | |
Powered by | 1 RD-1046D |
Maximum thrust | 68.6 kilonewtons (15,400 lbf)[1] |
Specific impulse | 463 sec[1] |
Burn time | 1,350 seconds |
Propellant | LH2/LOX |
The KVTK (Russian: Кислородно-водородный тяжёлого класса, Oxygen/Hydrogen Heavy Class) is a liquid Oxygen/Hydrogen upper stage booster for heavy-lift launch vehicle. The KVTK contains an RD-0146D engine and is designed for use on the Angara Rocket.[1] KVTK would be the first hydrogen-powered upper stage for use on a Russian launch vehicle, although Khrunichev has previously produced a hydrogen-powered upper stage KVD-1 for the Indian GSLV.[2] KVTK is designed to provide up to five ignitions, allowing for complex orbital maneuvering, and have an on-orbit lifespan of up to nine hours. KVTK would allow an increase in payload to GTO of 20-50% compared to the Angara A5's standard Briz-M upper stage, powered by UDMH and N2O4.[3]
Variants
The RCAF would be a smaller cryogenic stage carrying 10,760 kilograms (23,720 lb) of propellant for the proposed Angara A3,[4] while the KVSK-A7 would be a larger stage loaded with 26,500 kilograms (58,400 lb) for the proposed Angara A7.[5]
References
- ^ a b c d e f g "Angara A5". Spaceflight 101. Retrieved July 2014.
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(help) - ^ Zak, Anatoly (June 26, 2014). "KVTK to give hydrogen power to Angara". RussianSpaceWeb. Retrieved July 2014.
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(help) - ^ "Angara Launch Vehicles Family". khrunichev.ru. Retrieved July 2014.
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(help) - ^ "Angara A3". Spaceflight 101. Retrieved July 2014.
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(help) - ^ "KVTK". khrunichev.ru. Retrieved July 2014.
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