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Chang Zheng 2D
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CZ-2D |
Chinese orbital launch vehicle. The Long March 2D was a two-stage launch vehicle with storable propellants, suitable for launching a variety of low earth orbit satellites. Developed and manufactured by the Shanghai Academy of Spaceflight Technology, the CZ-2D had a typical payload capability of 3,500kg in a 200 km circular orbit. Its first stage was identical to that of the CZ-4. The second stage was essentially the same as that of the CZ-4, except for an improved vehicle equipment bay.
AKA: Chang Zheng-2D;CZ-2D;Long March 2D. Status: Active. First Launch: 1992-08-09. Last Launch: 2016-12-28. Number: 31 . Payload: 3,500 kg (7,700 lb). Thrust: 2,926.20 kN (657,836 lbf). Gross mass: 232,250 kg (512,020 lb). Height: 35.07 m (115.05 ft). Diameter: 3.35 m (10.99 ft). Apogee: 200 km (120 mi).
LEO Payload: 3,500 kg (7,700 lb) to a 200 km orbit at 28.00 degrees. Launch Price $: 15.000 million in 1999 dollars. Stage Data - CZ-2D - Stage 1. 1 x CZ-4A-1. Gross Mass: 192,700 kg (424,800 lb). Empty Mass: 9,500 kg (20,900 lb). Thrust (vac): 3,265.143 kN (734,033 lbf). Isp: 289 sec. Burn time: 170 sec. Isp(sl): 259 sec. Diameter: 3.35 m (10.99 ft). Span: 6.00 m (19.60 ft). Length: 24.66 m (80.90 ft). Propellants: N2O4/UDMH. No Engines: 4. Engine: YF-20B. Other designations: L-180. Status: In Production.
- Stage 2. 1 x CZ-4A-2. Gross Mass: 39,550 kg (87,190 lb). Empty Mass: 4,000 kg (8,800 lb). Thrust (vac): 831.005 kN (186,817 lbf). Isp: 295 sec. Burn time: 135 sec. Isp(sl): 260 sec. Diameter: 3.35 m (10.99 ft). Span: 3.35 m (10.99 ft). Length: 10.41 m (34.15 ft). Propellants: N2O4/UDMH. No Engines: 1. Engine: YF-25/23. Other designations: L-35. Status: In Production.
More at: Chang Zheng 2D.
Family: orbital launch vehicle.
Country: China.
Engines: YF-25/23,
YF-20B.
Spacecraft: Jilin,
CAST1000,
CAST2000,
Ling Qiao,
Proteus,
SJ-7,
Tianhui,
FSW,
SJ,
Cubesat,
CX-1,
Shiyan,
Zheda Pixing,
JB-6.
Launch Sites: Jiuquan,
Jiuquan LA2B,
Jiuquan SLS,
Jiuquan SLS-2.
Stages: CZ-4A-1,
CZ-4A-2.
Agency: CALT.
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