LR87plus

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

LR87plus

Part of LR87

Aerojet N2O4/Aerozine-50 rocket engine. Study 1965. Nominal improved LR87 in booster studies. Used on Martin Astrorocket launch vehicle.

Status: Study 1965. Thrust: 1,634.40 kN (367,428 lbf). Specific impulse: 293 s. Specific impulse sea level: 258 s. Burn time: 164 s.

Thrust (sl): 1,439.200 kN (323,545 lbf). Thrust (sl): 146,757 kgf.

Family: Storable liquid. Country: USA. Launch Vehicles: Martin Astrorocket. Propellants: N2O4/Aerozine-50. Stages: Astrorocket-1, Astrorocket-2. 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