Long March 8
Appearance
Function | Orbital launch vehicle |
---|---|
Manufacturer | China Academy of Launch Vehicle Technology (CALT) |
Country of origin | China |
Size | |
Height | 50.34 m (165.2 ft) |
Diameter | 3.35 m (11.0 ft) |
Width | 1.4 |
Mass | 356,000 kg (785,000 lb) |
Stages | 2 |
Capacity | |
Payload to SSO 700 km | |
Mass | 4,500 kg (9,900 lb) |
Payload to LEO | |
Mass | 8,400 kg (18,500 lb) |
Payload to GTO | |
Mass | 2,800 kg (6,200 lb) |
Associated rockets | |
Comparable | Soyuz-2 Antares Falcon 9 (RTLS reusable) Ariane 6 H3 |
Launch history | |
Status | Active |
Launch sites | Wenchang, LC-2 Jiuquan |
Total launches | 1 |
Success(es) | 1 |
First flight | 22 December 2020 |
Boosters – K2 booster | |
No. boosters | 2 |
Height | 26.903 m (88.26 ft) |
Diameter | 2.25 m (7 ft 5 in) |
Powered by | 1 YF-100 |
Maximum thrust | Sea level: 1,200 kN (270,000 lbf) Vacuum: 1,340 kN (300,000 lbf) |
Total thrust | Sea level: 4,800 kN (1,100,000 lbf) Vacuum: 5,360 kN (1,200,000 lbf) |
Specific impulse | Sea level: 300 s (2.9 km/s) Vacuum: 335 s (3.29 km/s) |
Propellant | RP-1 / LOX |
First stage – K3 core module | |
Height | 25.083 m (82.29 ft) |
Diameter | 3.35 m (11.0 ft) |
Powered by | 2 YF-100 |
Maximum thrust | Sea level: 2,400 kN (540,000 lbf) Vacuum: 2,680 kN (600,000 lbf) |
Specific impulse | Sea level: 300 s (2.9 km/s) Vacuum: 335 s (3.29 km/s) |
Propellant | RP-1 / LOX |
Second stage | |
Height | 12.375 m (40.60 ft) |
Diameter | 3.0 m (9.8 ft) |
Powered by | 2 YF-75 |
Maximum thrust | 167.17 kN (37,580 lbf) |
Specific impulse | 438 s (4.30 km/s) |
Propellant | LH2 / LOX |
Long March 8 (Chinese: 长征八号运载火箭) is an orbital launch vehicle developed by the China Academy of Launch Vehicle Technology to launch up to 4500 kg to a 700 km altitude Sun-synchronous orbit (SSO). The rocket is based on the Long March 7 with its first stage and 2 of its boosters, along with the existing liquid hydrogen burning third stage of the Long March 3A/3B/3C and 7A as its second stage.
A planned future launch vehicle variant of the Long March 8 will be partially reusable by featuring a combined booster recovery of the first stage and the boosters as a single unit.[1]
The maiden flight of the Long March 8 was launched on 22 December 2020 from the Wenchang Spacecraft Launch Site.
List of launches
Flight number | Date (UTC) |
Launch site | Payload | Orbit | Outcome |
---|---|---|---|---|---|
1 | 22 December 2020 04:37 |
Wenchang, LC-2 | Xinjishu Yanzheng 7 (XJY-7) Haisi-1 Tianqi Xingzuo 08 (Ping'an-1) Yuanguang-1 ET-SMART-RSS (Zhixing-1A) [2] |
SSO | Success [3] |
See also
- Comparison of orbital launchers families
- Comparison of orbital launch systems
- Expendable launch system
- Lists of rockets
References
- ^ Jones, Andrew. "China to test rocket reusability with planned Long March 8 launcher". SpaceNews. Retrieved 6 December 2020.
- ^ "China launches first Long March 8 from Wenchang spaceport". SpaceNews. 22 December 2020. Retrieved 22 December 2020.
- ^ "长征八号运载火箭首次飞行试验取得圆满成功". Retrieved 22 December 2020.