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Delta F
Part of Delta Family
Nitric acid/UDMH propellant rocket stage. .

Status: Retired 1987. Thrust: 41.36 kN (9,299 lbf). Gross mass: 5,629 kg (12,409 lb). Unfuelled mass: 784 kg (1,728 lb). Specific impulse: 280 s. Burn time: 335 s. Height: 6.28 m (20.60 ft). Diameter: 1.40 m (4.50 ft). Span: 1.40 m (4.50 ft).

Cost $ : 2.320 million.



Country: USA. Engines: AJ10-118F. Launch Vehicles: Delta 0900, Delta 1604, Delta 0300, Delta 1913, Delta 1900, Delta 1910, N-2, N-2 (2). Propellants: Nitric acid/UDMH.

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