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From Wikipedia, the free encyclopedia

BF-20
Country of originChina
ManufacturerLandSpace
StatusIn development
Liquid-fuel engine
PropellantLOX / CH4
Performance
Thrust, vacuum2,366 kilonewtons (532,000 lbf)
Thrust, sea-level2,200 kilonewtons (490,000 lbf)
Throttle range40%~120%
Chamber pressure26 MPa (3,800 psi)
Specific impulse, vacuum353.16s
Specific impulse, sea-level328.47s
Used in
ZQ-3
References
Notes[1]

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.

History

In 2021, LandSpace initiated the development of BF-20 for its Zhuque-3 rocket. As of 2024, the technical design of the engine has been completed, and a hot fire test is scheduled for 2025, with the goal of achieving flight readiness by 2027.[2][3]

References

  1. ^ Zhang, Xiaoping; Zhou, Yaqiang; Wei, Yan (2023-01-17). "Current State of LOX/Methane Engine Development - 液氧甲烷发动机发展现状". d.wanfangdata.com.cn (1): 126–133. doi:10.3969/j.issn.1674-5825.2023.01.017. Retrieved 22 May 2024.
  2. ^ Guo, Songjiao; Zhang, Yuhong (24 April 2024). "蓝箭样本:可重复使用火箭缘何选择液氧甲烷?". finance.sina.cn. Retrieved 22 May 2024.
  3. ^ Jones, Andrew (19 January 2024). "China's Landspace conducts first VTVL test for reusable stainless steel rocket". SpaceNews. Retrieved 22 May 2024.
This page was last edited on 30 May 2024, at 15:47
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