Computational studies to optimize the geometry of the low-thrust rocket combustion chamber using gaseous propellants
Authors: Novikov A.V., Andreev E.A., Bardakova E.I.
Published in issue: #11(119)/2021
DOI: 10.18698/2308-6033-2021-11-2129
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts