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Research of the effect of an extended-surface of the chamber cooling jacket on the performance parameters of an oxygen-hydrogen liquid-propellant rocket engine by expander cycle
| Authors: Belyakov V.A., Vasilevsky D.O., Romashko R.V. | Published: 28.01.2026 |
| Published in issue: #2(791)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: liquid-propellant rocket engine by expander cycle, mathematical model for calculating, intensification of heat transfer, specific impulse of the engine |
