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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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