Semi-open oxygen-rich staged combustion cycle liquid rocket engine
CN309984066SActive Publication Date: 2026-05-15SHAANXI TIANHUI AEROSPACE TECH CO LTD +1
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Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Designs(China)
- Current Assignee / Owner
- SHAANXI TIANHUI AEROSPACE TECH CO LTD
- Filing Date
- 2025-10-23
- Publication Date
- 2026-05-15
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Figure 000007_ABST
Abstract
1. The name of the design product: semi-open oxygen-enriched hypergolic cycle liquid rocket engine. 2. The use of the design product: the present design relates to a semi-open oxygen-enriched hypergolic cycle liquid rocket engine, which is used for driving liquid carrier rockets and aircraft. 3. The design points of the design product: in shape. 4. The picture or photo that best indicates the design points: perspective view.
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