Numerical study of the operating condition effect on the thermal state of the structure of low thruster on oxygen-methane propellant operating in pulsed mode
Published: 30.11.2016
Authors: Vorozheeva O.A., Yagodnikov D.A.
Published in issue: #1(61)/2017
DOI: 10.18698/2308-6033-2017-1-1570
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts