Innovative methodology for calculation and design of liquid-propellant rocket engine combustion chamber
Published: 21.11.2016
Authors: Korotkaya O.V.
Published in issue: #12(60)/2016
DOI: 10.18698/2308-6033-2016-12-1560
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts