T-7 LRE

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Engine Model: T-7 LRE. Designer: SIMED/Shanghai. Gross Mass: 1,000 kg (2,200 lb). Propellants: Solid. Diameter: 0.45 m (1.47 ft). Length: 6.00 m (19.60 ft). Country: China. T-7 LRE used on Rocket Stages Used on stage: T-7. on launch vehicle: T-7. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.