H-1c

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

H-1c

Part of LR79

Rocketdyne LOx/Kerosene rocket engine. Study Saturn IB-A, Saturn IB-B, 1965.

Status: Study 1965. Thrust: 1,130.00 kN (254,030 lbf). Specific impulse: 296 s. Specific impulse sea level: 262 s. Burn time: 128 s.

Country: USA. Launch Vehicles: Saturn IB-A, Saturn IB-B. Propellants: Lox/Kerosene. Stages: Saturn S-IB-A. 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