TQ-11
| Country of origin | China |
|---|---|
| Manufacturer | Landspace |
| Status | Under development |
| Liquid-fuel engine | |
| Propellant | Liquid oxygen / Liquefied natural gas |
| Configuration | |
| Nozzle ratio | 25.5 |
| Performance | |
| Thrust, vacuum | 80 kilonewtons (18,000 lbf) |
| Chamber pressure | 10.1 MPa (1,460 psi) |
| Specific impulse, vacuum | 337s |
| Dimensions | |
| Measurement | 1.1m |
| Diameter | 0.28m |
| Used in | |
| ZQ-2 | |
| References | |
| Notes | [1] |
The TQ-11 (Chinese: 天鹊-11; pinyin: Tiānquè-11, lit. Sky Lark 11) is a gas-generator cycle rocket engine burning liquid methane and liquid oxygen under development by Landspace. It will be used as the second stage vernier engine for Landspace's ZQ-2 rocket.[2][3][4] The engine has been designed to produce 80 kilonewtons (18,000 lbf) of thrust in the vacuum.[1] Landspace completed the first engine hot firing test for TQ-11 on November 3, 2019, and the engine passed a 1500 second test in 2020.[2][4]
References[]
- ^ a b "TQ-11 Engine". Landspace. Retrieved 4 March 2021.
- ^ a b "System-level Test Run for "TQ-11"LRE Successfully Conducted - Landspace". Landspace. Retrieved 22 March 2021.
- ^ "Will LandSpace be China's SpaceX?". The Space Review. Retrieved 23 March 2021.
- ^ a b Jones, Andrew (14 April 2020). "Space Pioneer raises $14 million to develop green liquid rocket engines". SpaceNews.
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| Solid fuel |
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