Long March 6

The Long March 6 (Chinese: 长征六号运载火箭) or Chang Zheng 6 as in pinyin, abbreviated LM-6 for export or CZ-6 within China, is a Chinese liquid-fuelled carrier rocket of the Long March family, which was developed by the China Aerospace Science and Technology Corporation[7] and the Shanghai Academy of Spaceflight Technology. The rocket was developed in the 2000s, and made its maiden flight in 2015.[8] As one of the new generation rocket family, the Long March 6 was designed to be a light capacity, "high-speed response" rocket, complementing the heavy lift Long March 5 and the mid-heavy lift Long March 7 rocket families. It is capable of placing at least 1,000 kilograms (2,200 lb) of payload into a sun-synchronous orbit.[9][8] The first stage of the Long March 6 was derived from the booster rockets being developed for the Long March 5 rocket. It is powered by a YF-100 engine, which generates 1,340 kilonewtons or 300,000 pounds-force of thrust from burning kerosene and LOX as rocket fuel and oxidiser.[8] This was the first flight of the new engine design.[3]

Long March 6
Maiden flight of Long March 6 rocket
FunctionSmall carrier rocket
ManufacturerSAST[1]
Country of originChina
Size
Height29 m (95 ft)
Diameter3.35 m (11.0 ft)
Mass103,000 kg (227,000 lb)
Stages3[2]
Capacity
Payload to 700 km (430 mi) SSO1,080 kilograms (2,380 lb)
Associated rockets
FamilyLong March
Long March 6
ComparableMinotaur-C, PSLV-CA
Launch history
StatusActive
Launch sitesLA-16, TSLC
Total launches3
Successes3
First flight19 September 2015[3]
First stage
Diameter3.35 m (11.0 ft)
Propellant mass61,000 kg (134,000 lb) to 76,000 kg (168,000 lb)
Engines1 YF-100
Thrust1,188 kN (267,000 lbf)[4]
Specific impulse300 sec (SL); 335 sec (Vac)[5]
FuelRP-1/LOX
Second stage
Diameter2.25 m (7.4 ft)
Propellant mass15,000 kg (33,000 lb)
Engines1 YF-115
Thrust180 kN (40,000 lbf)[4]
Specific impulse341.5 sec (Vac)[6]
FuelRP-1/LOX
Third stage
Diameter2.25 m (7.4 ft)
Engines1
Thrust6.5 kN (1,500 lbf)[4]
Specific impulse306.9 sec[4]
FuelN2O4 / UDMH[4]

A boosted variant, with a payload of 4 tons to sun-synchronous orbit, is under development.

List of launches

Flight number Date (UTC) Launch site Payload Orbit Result
1 September 19, 2015
23:01
LA-16, TSLC ZDPS-2A
ZDPS-2B
NS-2
ZJ-1
ZJ-2
Tiantuo 3
NUDT-Phone-Sat
Xingchen 1
Xingchen 2
Xingchen 3
Xingchen 4
LilacSat 2
XY-2
DCBB
Xiwang-2A
Xiwang-2B
Xiwang-2C
Xiwang-2D
Xiwang-2E
Xiwang-2F
SSO Success[8]
2 November 21, 2017
04:50
LA-16, TSLC Jilin-1 04
Jilin-1 05
Jilin-1 06
SSO Success
3 November 13, 2019
06:35
LA-16, TSLC Ningxia-1 01
Ningxia-1 02
Ningxia-1 03
Ningxia-1 04
Ningxia-1 05
LEO Success

See also

References

  1. "China conducts debut launch of Long March 6". NASASpaceflight. Retrieved 2015-09-19.
  2. "突破运力"下限"的长征6号" [Advances in Light Capacity Long March 6] (in Chinese). Tencent Military Channel. 2013-12-19. Retrieved 2015-08-03.
  3. The Long March 6 launched a 20-star in Taiyuan to create the best in Asia. in Chinese
  4. ZHANG Wei-dong, WANG Dong-bao (2016). "New Generation Cryogenic Quick Launching Launch Vehicle and Development". AEROSPACE SHANGHAI.
  5. "Chinese YF-100 (Russian RD-120) to Power CZ-5". SPACEPAC, The Space Public Affairs Committee. Retrieved 2015-07-02.
  6. "中国新一代液氧煤油发动机3:YF100/115主要特性 - 深空网". www.shenkong.net (in Chinese). Archived from the original on 2016-03-04. Retrieved 2016-04-11.
  7. "Development of China's new "Changzheng 6" carrier rocket commences". People's Daily Online. 2009-09-04. Retrieved 2009-09-06.
  8. "China conducts debut launch of Long March 6". 2015-09-19. Retrieved 2015-09-20.
  9. "Archived copy". Archived from the original on 2015-09-18. Retrieved 2015-09-20.CS1 maint: archived copy as title (link)


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