Experimental evaluation of rational parameters of pre-acceleration to ensure liquid sustainer engine launch in zero gravity
Published: 26.09.2019
Authors: Sapozhnikov V.B., Polyanskiy A.R., Korolkov A.V.
Published in issue: #9(93)/2019
DOI: 10.18698/2308-6033-2019-9-1916
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts