Experimental estimation of residual propellant in the fuel tanks with innertank capillary devices for spacecraft propulsion systems
Published: 10.12.2019
Authors: Sapozhnikov V.B., Polyanskiy A.R., Korolkov A.V., Konstantinov S.B., Alexandrov L.G.
Published in issue: #12(96)/2019
DOI: 10.18698/2308-6033-2019-12-1941
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts