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The Influence of Thrust Chamber Structure Parameters on Regenerative Cooling Effect with Hydrogen Peroxide as Coolant in Liquid Rocket Engines.
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- Aerospace (MDPI Publishing), 2023, v. 10, n. 1, p. 65, doi. 10.3390/aerospace10010065
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Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine.
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- Scientific Reports, 2023, v. 13, n. 1, p. 1, doi. 10.1038/s41598-023-43259-8
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- Publication type:
- Article
Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine.
- Published in:
- Scientific Reports, 2023, v. 13, n. 1, p. 1, doi. 10.1038/s41598-023-43259-8
- By:
- Publication type:
- Article