Calculation of minimum supply of fuel in contact with the innertank device to ensure the operation of a liquid-propellant rocket engine in zero gravity
Published: 24.03.2021
Authors: Sapozhnikov V.B., Polyanskiy A.R., Korolkov A.V.
Published in issue: #3(111)/2021
DOI: 10.18698/2308-6033-2021-3-2063
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts