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Family: Long March. Country: China. Status: Hardware. Other Designations: Long March 1M.
Proposed launch vehicle derived from CZ-1, with an Italian Mage upper stage. Never flown.
SpecificationsLiftoff Thrust: 112,290 kgf. Total Mass: 80,930 kg. Core Diameter: 2.3 m. Total Length: 31.0 m.
- Stage Number: 1. 1 x CZ-1-1 Gross Mass: 64,100 kg. Empty Mass: 4,100 kg. Thrust (vac): 124,872 kgf. Isp: 268 sec. Burn time: 130 sec. Isp(sl): 241 sec. Diameter: 2.3 m. Span: 4.0 m. Length: 17.8 m. Propellants: Nitric acid/UDMH No Engines: 4. YF-2A
- Stage Number: 2. 1 x CZ-1-2 Gross Mass: 15,000 kg. Empty Mass: 2,700 kg. Thrust (vac): 31,218 kgf. Isp: 275 sec. Burn time: 110 sec. Isp(sl): 200 sec. Diameter: 2.3 m. Span: 2.3 m. Length: 5.4 m. Propellants: Nitric acid/UDMH No Engines: 1. YF-2A
- Stage Number: 3. 1 x CZ-1M-3 Gross Mass: 1,830 kg. Empty Mass: 256 kg. Thrust (vac): 3,000 kgf. Isp: 291 sec. Burn time: 150 sec. Isp(sl): 115 sec. Diameter: 1.3 m. Span: 1.3 m. Length: 2.3 m. Propellants: Solid No Engines: 1. Iris
Bibliography:- 42 - Isakowitz, Steven J,, International Reference to Space Launch Systems Second Edition, AIAA, Washington DC, 1991.
- 61 - Wilson, Andrew, editor,, Jane's/Interavia Space Directory, Jane's Information Group, Coulsdon, Surrey, 1992 et al.
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Last update 12 March 2001.
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© Mark Wade, 2001 .