The patent application relates to the design of a ramjet engine whereby air injection ports and fuel injection systems are arranged in a manner to enhance flame stability.
Integral Rocket/Ramjet Propulsion System with Axial Admission Ports
1974
17 pages
Report
No indication
English
Propulsion System Analysis and Flight Test of an Integral Rocket Ramjet
British Library Conference Proceedings | 1995
|Liquid fueled integral rocket/ramjet technology review
AIAA | 1978
|