AJ10-137

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

AJ10-137

Part of AJ10

Aerojet N2O4/Aerozine-50 rocket engine. Apollo SPS. Out of Production. Pressure-fed engine. Used as Apollo SM engine.

Status: Out of Production. Thrust: 97.50 kN (21,919 lbf). Specific impulse: 312 s. Burn time: 585 s.

Chamber Pressure: 6.90 bar. Oxidizer to Fuel Ratio: 1.6.

Family: Storable liquid. Country: USA. Spacecraft: Apollo CSM, Apollo CSM Block I, Apollo RM. Propellants: N2O4/Aerozine-50. Agency: Aerojet.

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