LR91-9

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

LR91-9

Part of LR91

Aerojet N2O4/Aerozine-50 rocket engine. Titan III B, C, D. Out of Production. Version used in earlier versions of Titan 3 upper stages. First flight 1965.

AKA: AJ23-137. Status: Out of Production. Date: 1968. Thrust: 448.61 kN (100,850 lbf). Specific impulse: 316 s.

Family: Storable liquid. Country: USA. Launch Vehicles: Titan IIIC, Titan IIIB, Titan IIID. 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