Zhuque-2
Rendering of Zhuque-2 | |
| Function | Orbital launch vehicle |
|---|---|
| Manufacturer | LandSpace |
| Country of origin | China |
| Size | |
| Height | Zhuque-2: 49.5 m (162 ft) Zhuque-2E: 47.3 m (155 ft) |
| Diameter | 3.35 m (11.0 ft) |
| Mass | 219,000 kg (483,000 lb) |
| Stages | 2 |
| Capacity | |
| Payload to low Earth orbit (LEO) 200 km | |
| Mass | Zhuque-2: 4,000 kg (8,800 lb) Zhuque-2E: 6,000 kg (13,000 lb) |
| Payload to Sun-synchronous orbit (SSO) | |
| Mass | Zhuque-2: 1,500 kg (3,300 lb) Zhuque-2E: 4,000 kg (8,800 lb) |
| Launch history | |
| Status |
|
| Launch sites |
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| Total launches |
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| Success(es) |
|
| Failure(s) | 1 |
| First flight |
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| Last flight | 17 May 2025 |
| First stage | |
| Powered by | 4 × TQ-12 |
| Maximum thrust | 2,680 kN (273 tf; 600,000 lbf) |
| Propellant | LOX / CH4 |
| Second stage | |
| Powered by | Zhuque-2: 1 × TQ-12 Vac
1 × TQ-11 (Vernier) Zhuque-2E: 1 × TQ-15A |
| Maximum thrust |
|
| Propellant | LOX / CH4 |
Zhuque-2 (Chinese: 朱雀二号; pinyin: Zhūquè èr hào; lit. 'Vermilion Bird-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.