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Delta K
Part of Delta
N2O4/Aerozine-50 propellant rocket stage. .
Status: Active. Thrust: 43.63 kN (9,808 lbf). Gross mass: 6,954 kg (15,330 lb). Unfuelled mass: 950 kg (2,090 lb). Specific impulse: 319 s. Burn time: 431 s. Height: 5.89 m (19.32 ft). Diameter: 1.70 m (5.50 ft). Span: 2.40 m (7.80 ft).
Cost $ : 4.350 million.
Country:
USA.
Engines:
AJ10-118K.
Launch Vehicles:
Delta 3920,
Delta 3920/PAM,
Delta 3924,
Delta 4000,
Delta 5000,
Delta 6925,
Delta 3920-8,
Delta 4925-8,
Delta 5920-8,
Delta 6920-8,
Delta 6925-8,
Delta 6920-10,
Delta 7925,
Delta 7925-8,
Delta 7925-10,
Delta 7920-10,
Delta 7920-10C,
Delta 7920-8,
Delta 7925-9.5,
Delta 7420-10C,
Delta 7326-9.5,
Delta 7425-9.5,
Delta 7426-9.5,
Delta 7320-10,
Delta 7425-10,
Delta 7920-10L,
Delta 7920H,
Delta 7320-10C,
Delta 7925-10L,
Delta 7925H,
Delta IV Small.
Propellants:
N2O4/Aerozine-50.
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