Chinese orbital launch vehicle
Long March 4B Rendering of Long March 4B
Function Launch vehicle Manufacturer SAST Country of origin China Cost per launch US$50 million (2006) [1] Height 44.1 m (145 ft)[ 1] Diameter 3.35 m (11.0 ft)[ 2] Mass 249,200 kg (549,400 lb)[ 2] Stages 3 Mass 4,200 kg (9,300 lb) [ 3] Mass 2,800 kg (6,200 lb)[ 3] Mass 1,500 kg (3,300 lb)[ 3]
Family Long March Derivative work Long March 4C Status Active Launch sites Total launches 52 Success(es) 51 Failure(s) 1 First flight 10 May 1999 Last flight 13 November 2024 Height 27.91 m (91.6 ft) Diameter 3.35 m (11.0 ft) Propellant mass 182,000 kg (401,000 lb) Powered by 4 YF-21C Maximum thrust 2,961.6 kN (665,800 lbf ) Specific impulse 2,550 m/s (8,400 ft/s) Propellant N2 O4 / UDMH Height 10.9 m (36 ft) Diameter 3.35 m (11.0 ft) Propellant mass 52,700 kg (116,200 lb) Powered by 1 YF-24C (1 x YF-22C (Main)) (4 x YF-23C (Vernier)) Maximum thrust 742.04 kN (166,820 lbf ) (Main) 47.1 kN (10,600 lbf ) (Vernier) Specific impulse 2,942 m/s (9,650 ft/s) (Main) 2,834 m/s (9,300 ft/s) (Vernier) Propellant N2 O4 / UDMH Height 14.79 m (48.5 ft) Diameter 2.9 m (9 ft 6 in) Propellant mass 14,000 kg (31,000 lb) Powered by 2 YF-40 Maximum thrust 100.85 kN (22,670 lbf ) Specific impulse 2,971 m/s (9,750 ft/s) Propellant N2 O4 / UDMH
The Long March 4B (Chinese : 长征四号乙火箭 ), also known as the Chang Zheng 4B , CZ-4B , and LM-4B , is a Chinese expendable orbital launch vehicle . Launched from Launch Complex 1 at the Taiyuan Satellite Launch Center , it is a 3-stage launch vehicle, used mostly to place satellites into low Earth orbit and Sun-synchronous orbits . It was first launched on 10 May 1999, with the FY-1C weather satellite, which would later be the target in the 2007 Chinese anti-satellite missile test .
The Chang Zheng 4B experienced its only launch failure on 9 December 2013, with the loss of the CBERS-3 satellite.[ 4]
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List of launches
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