Wikiwand AI

Zhuque-2

Orbital launch vehicle by LandSpace From Wikipedia, the free encyclopedia

Zhuque-2 (Chinese: 朱雀二号; pinyin: Zhūquè èr hào; lit. 'Zhuque-2', ZQ-2) is a Chinese medium-class orbital launch vehicle developed by LandSpace. It is a liquid-fuelled rocket powered by liquid oxygen and liquid methane (methalox) and was the first methane-fueled rocket to reach orbit.[2][3]

ManufacturerLandSpace
Country of originChina
Height
  • Zhuque-2: 49.5 m (162 ft)
  • Zhuque-2E (block 1): 47.8 m (157 ft)
  • Zhuque-2E (block 2): 55.9 m (183 ft)[1]
Quick facts Function, Manufacturer ...
Zhuque-2
Rendering of Zhuque-2
FunctionOrbital launch vehicle
ManufacturerLandSpace
Country of originChina
Size
Height
  • Zhuque-2: 49.5 m (162 ft)
  • Zhuque-2E (block 1): 47.8 m (157 ft)
  • Zhuque-2E (block 2): 55.9 m (183 ft)[1]
Diameter3.35 m (11.0 ft)
Mass
  • Zhuque-2: 219,000 kg (483,000 lb)
  • Zhuque-2E (block 1): 220,000 kg (490,000 lb)
  • Zhuque-2E (block 2): 267,000 kg (589,000 lb)
Stages2
Capacity
Payload to LEO
Altitude200 km (120 mi)
MassZhuque-2: 4,000 kg (8,800 lb)
Zhuque-2E: 6,000 kg (13,000 lb)[1]
Payload to SSO
MassZhuque-2: 1,500 kg (3,300 lb)
Zhuque-2E: 4,000 kg (8,800 lb)[1]
Launch history
Status
  • Zhuque-2: Retired
  • Zhuque-2E: Active
Launch sites
Total launches10
Success(es)8
Failure2
First flight14 December 2022
Last flight14 October 2026, most recent
First stage
Powered by
Maximum thrust
  • Zhuque-2: 2,680 kN (273 tf; 600,000 lbf)
  • Zhuque-2E (block 1): 2,880 kN (294 tf; 650,000 lbf)
  • Zhuque-2E (block 2): 3,312 kN (337.7 tf; 745,000 lbf)
PropellantLOX / CH4
Second stage
Powered by
Maximum thrust
  • Zhuque-2: 777.67 kN (79.300 tf; 174,830 lbf)
  • Zhuque-2E: 836 kN (85.2 tf; 188,000 lbf)
PropellantLOX / CH4
Close
Zhuque-2 Launch

Design

Zhuque-2 has a liftoff weight of 216 tonnes and uses 4 TQ-12 methalox engines in the first stage, each with a thrust of 67 tonnes-force (660 kN).[4][5] The second stage uses one vacuum-optimized TQ-12 with a thrust of 80 tonnes-force (780 kN) in combination with a TQ-11 engine (8 tonnes-force (78 kN) thrust), which acts as a vernier thruster.[6]

Zhuque-2 is capable of lifting 6,000 kg of payload into a 200 km low Earth orbit and 4,000 kg of payload into a 500 km Sun-synchronous orbit.[2][7]

History

In May 2019, LandSpace performed test firings of its liquid-methane and liquid-oxygen fuelled TQ-12 rocket engine at its test facility at Huzhou, Zhejiang province. LandSpace's head of research and development, Ge Minghe, says that the engine has a thrust of 80 tonnes-force. The Huzhou facility will be able to produce about 15 ZQ-2 rockets and 200 TQ-12 engines starting in 2022, according to CEO, Zhang Changwu.[8][9][needs update]

On 14 December 2022, LandSpace conducted the debut flight of Zhuque-2, but failed to reach orbit due to an early shutdown of its second-stage vernier engines after the second-stage main engines apparently completed a successful burn. It was the world's first orbital launch attempt by a methane-fueled launch vehicle.[10]

In March 2023, LandSpace confirmed that the second Zhuque-2 launch vehicle had completed assembly and was undergoing preparations for a launch attempt in the coming months.[11]

On 12 July 2023, Zhuque-2 became the first methane-fueled launch vehicle to reach orbit after a successful second flight.[2][12]

Variant

Zhuque-2E

Bluish-white streaks, like the tail of a comet, glow in the night sky over a dark site over silhouetted trees and red lights from astronomers.
Dumped methalox propellant from the upper stage of Zhuque-2E flight Y5, rendered visible by sunlight

An enhanced version of the rocket, the Zhuque-2E, successfully placed two satellites into orbit on 27 November 2024. The new version of the rocket differs from the initial variant by featuring a common bulkhead tank structure, a new TQ-15 liquid oxygen and methane engine with thrust vectoring capabilities on the second stage, and a new niobium alloy nozzle extension on the enhanced TQ-15A engine.[13]

ZQ-2E (Block 2)

The Zhuque-2E (Y5), launched on 14 May 2026, is the first of the Block 2 subvariant of the launch vehicle. Various improvements were included on the Block 2 variant which allow the launch vehicle to reach its full designed capabilities such as lifting 6,000 kg (13,000 lb) to Low Earth orbit and 4,000 kg (8,800 lb) to a 500 kilometre SSO orbit. Improvements over the base ZQ-2E include: lengthened first-stage tanks, full subcooled propellant loading, a three-ignition second stage allowing orbital disposal, and an accelerated launch campaign and launch cycle. According to Spacenews.com, the 14 May 2026 article wrote, "...launch successfully inserted a 2,800-kilogram customized payload described as a 'large-scale constellation deployment experiment' into a 900-kilometer polar orbit, ... The mission demonstrated high-mass payload launch capability and readiness for multi-satellite launch services, the company said in a post-launch statement, as it looks to secure launch contracts from China’s megaconstellation projects."[1]

Launch statistics

Launch outcomes

1
2
3
4
'22
'23
'24
'25
'26
'27
  •   Failure
  •   Partial failure
  •   Success
  •   Planned

Launches

Zhuque-2 Y2 launch
More information Flight No., Rocket, serial ...
Close

See also

References

Related Articles

Timelines

Top Qs

Fact Checks