Characteristic Pilot Study of a Blended Fuel Ignition Gas-Dynamic System as Applied to Liquid-Propellant Rocket Thrusters
Published: 20.12.2012
Authors: Voronetskiy A.V., Arefiev K.Yu., Ilchenko M.A.
Published in issue: #10(10)/2012
DOI: 10.18698/2308-6033-2012-10-385
Category: Engineering | Chapter: Power engineering