Rendering of Long March 8 Y1 | |
Function | Orbital launch vehicle |
---|---|
Manufacturer | China Academy of Launch Vehicle Technology (CALT) |
Country of origin | China |
Size | |
Height |
|
Diameter | 3.35 m (11.0 ft) |
Mass |
|
Stages | 2 |
Capacity | |
Payload to SSO 700 km |
|
Payload to LEO | 8,100 kg (17,900 lb) |
Payload to GTO | 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 | 2 |
Successes | 2 |
First flight | 22 December 2020 |
Last flight | 27 February 2022 |
Boosters (Standard) – K2 booster | |
No. boosters | 2 or 0 |
Length | 26.903 m (88.26 ft) |
Diameter | 2.25 m (7 ft 5 in) |
Engines | 1 YF-100 |
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) |
Fuel | RP-1 / LOX |
First stage – K3 core module | |
Length | 25.083 m (82.29 ft) |
Diameter | 3.35 m (11.0 ft) |
Engines | 2 YF-100 |
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) |
Fuel | RP-1 / LOX |
Second stage | |
Length | 12.375 m (40.60 ft) |
Diameter | 3.0 m (9.8 ft) |
Engines | 2 YF-75 |
Thrust | 167.17 kN (37,580 lbf) |
Specific impulse | 438 s (4.30 km/s) |
Fuel | 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 5000 kg to a 700 km altitude Sun-synchronous orbit (SSO).[2] The rocket is based on the Long March 7 with its first stage and two boosters, along with the existing liquid hydrogen burning third stage of the Long March 3A/3B/3C and 7A as its second stage. The boosters are omitted in the "core only" variant that first flew on its second launch in February 2022.[1]
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.[3]
The maiden flight of the Long March 8 was launched on 22 December 2020 from the Wenchang Spacecraft Launch Site.[4]
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Flight number | Date (UTC) |
Variant | Launch site | Payload | Orbit | Outcome |
---|---|---|---|---|---|---|
1 | 22 December 2020 04:37[4][5] |
Standard | Wenchang, LC-2 | Xinjishu Yanzheng 7 (XJY-7) Haisi-1 Tianqi Xingzuo 08 (Ping'an-1) Yuanguang-1 ET-SMART-RSS (Zhixing-1A) |
SSO | Success |
2 | 27 February 2022 03:06[6] |
Core only[6] | Wenchang, LC-2 | Dayun (Xingshidai-17) Hainan-1 01, 02 Jilin-1 Gaofen-03D 10–18 Jilin-1 Mofang-02A 01 Qimingxing-1 Taijing-3 01 Taijing-4 01 Tianxian-1 (Chaohu-1) Chuangxing Leishen Wenchang-1 01, 02 XD-1 Tianqi-19 |
SSO | Success |
3 | 18 March 2024[7] | Standard | Wenchang, LC-2 | Queqiao-2 Tiandu-1, 2 |
Selenocentric | Planned |
Original source: https://en.wikipedia.org/wiki/Long March 8.
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