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DF-1-1
Part of A-4 Family
LOx/Alcohol rocket stage. 270.00 kN (60,698 lbf) thrust. Mass 14,000 kg (30,865 lb).

Status: Retired 1970's. Thrust: 270.00 kN (60,690 lbf). Gross mass: 14,000 kg (30,000 lb). Unfuelled mass: 4,000 kg (8,800 lb). Burn time: 65 s. Height: 14.10 m (46.20 ft). Diameter: 1.65 m (5.41 ft).



Country: China. Engines: DF-1 engine. Launch Vehicles: DF-1. Propellants: Lox/Alcohol. Agency: CALT.

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