Abstract
Abstract—The possibility of creating an environmentally safe self-igniting fuel mixture for liquid-propellant rocket engines is investigated. The mixture is based on kerosene with pyrophoric additives and an oxidant: highly concentrated hydrogen-peroxide solution. The self-ignition of the components is studied experimentally. Tests are also conducted in the combustion chamber of a low-thrust liquid-propellant rocket engine.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Published version (
Free)
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
