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Status: Development cancelled 1955.. Date: 1950. Thrust: 533.70 kN (119,981 lbf). Specific impulse: 245 s. Specific impulse sea level: 245 s. Thrust and specific impulse values are at sea level. Two would have been installed per booster. Cancelled in favor of a version of it burning kerosene instead of alcohol fuel, the LR-83.
Thrust (sl): 533.700 kN (119,981 lbf). Thrust (sl): 54,422 kgf.
Country: USA. Propellants: Lox/Alcohol. Agency: Rocketdyne. Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z � 1997-2016 Mark Wade - Contact � / Conditions for Use |
