Encyclopedia Astronautica
Soyuz 11A511U2-0

Lox/Kerosene propellant rocket stage. Loaded/empty mass 42,810/3,550 kg. Thrust 996.30 kN. Vacuum specific impulse 314 seconds.

Cost $ : 5.000 million.

Status: Retired 1996.
Gross mass: 42,810 kg (94,370 lb).
Unfuelled mass: 3,550 kg (7,820 lb).
Height: 19.60 m (64.30 ft).
Diameter: 2.68 m (8.79 ft).
Span: 2.68 m (8.79 ft).
Thrust: 996.30 kN (223,977 lbf).
Specific impulse: 314 s.
Specific impulse sea level: 257 s.
Burn time: 118 s.
Number: 416 .

More... - Chronology...

Associated Countries
Associated Engines
  • RD-107-11D511P Glushko Lox/Kerosene rocket engine. 996.4 kN. Soyuz 11A511U2-0. Out of production. OKB Glushko. Used on 11A511U2 Stage 0. Propellants kerosene (RG-1) / Lox. Diameter is per chamber. Isp=314s. First flight 1982. More...

Associated Launch Vehicles
  • Soyuz 11A511U2 Russian orbital launch vehicle. Soyuz 11A511U2 used synthetic kerosene ('Sintin') in first stage for launch of premium reconnaisance satellite and manned payloads requiring just a bit more payload than the standard 11A511 could offer. Further use of the 11A511U2 abandoned in 1996 due to Sintin production stoppage. Later Soyuz spacecraft launched on standard Soyuz, with reduced payload and rendezvous with Mir in lower orbit accepted. More...

Associated Propellants
  • Lox/Kerosene Liquid oxygen was the earliest, cheapest, safest, and eventually the preferred oxidiser for large space launchers. Its main drawback is that it is moderately cryogenic, and therefore not suitable for military uses where storage of the fuelled missile and quick launch are required. In January 1953 Rocketdyne commenced the REAP program to develop a number of improvements to the engines being developed for the Navaho and Atlas missiles. Among these was development of a special grade of kerosene suitable for rocket engines. Prior to that any number of rocket propellants derived from petroleum had been used. Goddard had begun with gasoline, and there were experimental engines powered by kerosene, diesel oil, paint thinner, or jet fuel kerosene JP-4 or JP-5. The wide variance in physical properties among fuels of the same class led to the identification of narrow-range petroleum fractions, embodied in 1954 in the standard US kerosene rocket fuel RP-1, covered by Military Specification MIL-R-25576. In Russia, similar specifications were developed for kerosene under the specifications T-1 and RG-1. The Russians also developed a compound of unknown formulation in the 1980's known as 'Sintin', or synthetic kerosene. More...

Home - Browse - Contact
© / Conditions for Use