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.
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). 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. 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.
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. 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. 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. On 12 July 2023, Zhuque-2 became the first methane-fueled launch vehicle to reach orbit after a successful second flight.
variant
Zhuque-2E
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.
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."
Launch statistics
Launch outcomes
Launches
See also
Comparison of orbital launcher families Comparison of orbital launch systems Expendable launch system Lists of rockets
References




