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Project 921-1
Part of Project 921 Family
Proj 921 Spacecraft
Proj 921 Spacecraft
Chinese Project 921 Spacecraft. Provisional drawing based on description and drawing of earlier design. Four solar panels, Soyuz-shaped re-entry vehicle, cylindrical forward orbital module, androgynous docking system.
LOx/Kerosene propellant rocket stage. Engine chamber pressure 13 to 15 MPa.

Status: Design 1992. Thrust: 5,406.14 kN (1,215,349 lbf). Gross mass: 306,000 kg (674,000 lb). Unfuelled mass: 20,000 kg (44,000 lb). Specific impulse: 330 s. Specific impulse sea level: 293 s. Burn time: 170 s. Height: 29.00 m (95.00 ft). Diameter: 4.50 m (14.70 ft). Span: 7.50 m (24.60 ft).

No Engines: 4.



Country: China. Launch Vehicles: Chang Cheng 1, Project 921. Propellants: Lox/Kerosene.

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