Ensuring reliable cooling of the combustion chamber of an oxygen-hydrogen liquid rocket engine of the first stage launcher with deep thrust throttling
Published: 19.01.2022
Authors: Mukambetov R.Ya., Borovik I.N.
Published in issue: #1(121)/2022
DOI: 10.18698/2308-6033-2022-1-2146
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts