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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.

AKA: 4K44;Progress;Shaddock/Sepal;SS-N-3c. Date: 1959. Thrust: 222.31 kN (49,977 lbf). Gross mass: 4,500 kg (9,900 lb). Specific impulse: 234 s. Specific impulse sea level: 234 s. Height: 10.00 m (32.00 ft). Diameter: 0.90 m (2.95 ft). Span: 2.59 m (8.50 ft).

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



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

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