| Country of origin | China |
|---|---|
| Manufacturer | LandSpace |
| Status | In development |
| Liquid-fuel engine | |
| Propellant | LOX / CH4 |
| Mixture ratio | 3.6 (±8%) (adjustable) |
| Cycle | Full-flow staged combustion |
| Performance | |
| Thrust, vacuum | 2,366 kilonewtons (532,000 lbf) |
| Thrust, sea-level | 2,200 kilonewtons (490,000 lbf) |
| Throttle range | 40%~120% |
| Chamber pressure | 26 MPa (3,800 psi) |
| Specific impulse, vacuum | 353.16s |
| Specific impulse, sea-level | 328.47s |
| Used in | |
| ZQ-3 | |
| References | |
| Notes | |
The BF-20 (Chinese: 蓝焱-20; pinyin: Lányàn-20, lit. Blue Flame 20) is a full-flow staged combustion cycle rocket engine burning liquid methane and liquid oxygen under development by LandSpace.
The engine uses two preburners: a fuel-rich preburner drives the fuel pump, while an oxygen-rich preburner drives the oxidizer pump. The exhaust from both preburners enters the main combustion chamber.
In 2021, LandSpace initiated the development of BF-20 for its Zhuque-3 rocket. By 2024, the technical design of the engine had been completed, with a hot-fire test planned for 2025 and flight readiness targeted for 2027.
The engine conducted its first full-system test in May 2025. By September 2025, it had completed thirty test firings, with thrust limited to 110 tons. In March 2026, LandSpace announced that the engine had completed a full-system long-duration test and over one hundred full-system ignition tests in total.