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P-7
P-7
P-7
Credit: Boeing / Rocketdyne
Rocketdyne N2O4/Aerozine-50 rocket engine. Aspen Booster. Pressure-fed. Thrust from 12,000 lb to 50,000 lb at sea level.

Date: 1959. Thrust: 222.31 kN (49,977 lbf). Specific impulse: 234 s. Specific impulse sea level: 234 s.

Thrust (sl): 222.310 kN (49,977 lbf). Thrust (sl): 22,670 kgf.

Family: Storable liquid. Country: USA. Propellants: N2O4/Aerozine-50. Agency: Rocketdyne. More at: 11596.



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