Long March 1

Chang Zheng-1
by GW_Simulations

Country of Origin: China
Manufacturer: MAI, CASC, CAST

Height: 29.86 m
Diameter: 2.25 m
Payload to LEO: 300 kg (LM-1), 930 kg (LM-1D
Total Mass: 81.57 tons

Launch Sites: Jiuquan
First Flight: April 24, 1970 (LM-1), June 1, 1995 (LM-1D)
Last Flight: March 3, 1971, January 3, 2002 (LM-1D)
Total Launches: 2 (LM-1), 3 (LM-1D)
Successful Launches: 2 (LM-1), 2 (LM-1D)

 

 

Long March 1

Stage Diameter Fuel Engine Time Thrust (Vac.) ISP (SL / Vac.) Mass / Empty Mass
1 (YF-2A) 2.25 m UDMH/AK27S 4 x YF-1A 130 s 4 x 303.6 kN 242.5 / 267.4 s 65.25 tons / 4.18 tons
2 2.25 m UDMH/AK27S YF-3A 126 s 320.2 kN ? / 286.9 s 13.55 tons / 2.34 tons
3 (FG-02) 0.77 m Solid FG-02 38 s 181 kN ? / 254 s 2.2 tons / 0.4 tons
WordPress Table

 

 

Long March 1D

Stage Diameter Fuel Engine Time Thrust (Vac.) ISP (SL / Vac.) Mass / Empty Mass
1 (YF-2B) 2.25 m UDMH/N2O4 4 x YF-1B 131.5 s 4 x 303.6 kN 242.5 / 267.4 s 65.25 tons / 4.1 tons
2 2.25 m UDMH/N2O4 2 x YF-40 365 s 98.1 kN ? / 295.2 s 14 tons / 1.62 tons
3 2.05 m HTPB FG-36 43 s 44 kN ? / 289 s 1.315 tons / 0.665 tons
WordPress Table

 

 

Links:

b14643.de

Wikipedia

Destination Orbite

Space Launch Report

Encyclopedia Astronautica

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