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Delta F
Part of Delta
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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