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AJ10-118F
Part of AJ10 Family
Aerojet Nitric acid/UDMH rocket engine. Used on Delta upper stage for Delta 0100, Delta 1000, N-2 boosters. First flight 1972.

Number: 13 . Thrust: 41.40 kN (9,307 lbf). Unfuelled mass: 95 kg (209 lb). Specific impulse: 306 s. Burn time: 335 s. Diameter: 1.40 m (4.50 ft).

Engine: 95 kg (209 lb). Chamber Pressure: 9.00 bar. Area Ratio: 40. Propellant Formulation: RFNA/UDMH. Thrust to Weight Ratio: 44.4. Coefficient of Thrust vacuum: 4.71652202294704. Coefficient of Thrust sea level: .27.



Family: Storable liquid. Country: USA. Launch Vehicles: N-2, Delta 0100, Delta 1000. Propellants: Nitric acid/UDMH. Stages: Delta F. Agency: Aerojet.

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