Computational and experimental study of reliability of rocket-engine firing and starting operation of low thruster on the gaseous components oxygen + methane with electric spark ignition
Published: 27.03.2017
Authors: Andreev E.A., Novikov A.V., Shatsky O.E.
Published in issue: #4(64)/2017
DOI: 10.18698/2308-6033-2017-4-1606
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts