Integral Rocket Ramjet Demonstration Programme (IRRDP)
Title | Integral Rocket Ramjet Demonstration Programme (IRRDP) PDF eBook |
Author | R.F. Calzone |
Publisher | |
Pages | 36 |
Release | 1998 |
Genre | |
ISBN |
Integral Rocket-ramjet Component Evaluation Test Program (U).
Title | Integral Rocket-ramjet Component Evaluation Test Program (U). PDF eBook |
Author | C. E. Franklin |
Publisher | |
Pages | 174 |
Release | 1975 |
Genre | Combustion |
ISBN |
(U) Integral Rocket-ramjet Component Evaluation Test Program
Title | (U) Integral Rocket-ramjet Component Evaluation Test Program PDF eBook |
Author | C. E. Franklin |
Publisher | |
Pages | 642 |
Release | 1973 |
Genre | Combustion |
ISBN |
Investigation of a Medium Range Air-to-air Integral Rocket/ramjet Missile
Title | Investigation of a Medium Range Air-to-air Integral Rocket/ramjet Missile PDF eBook |
Author | |
Publisher | |
Pages | |
Release | 1976 |
Genre | Air-to-air missiles |
ISBN |
Integral Rocket/Ramjet Propulsion System with Axial Admission Ports
Title | Integral Rocket/Ramjet Propulsion System with Axial Admission Ports PDF eBook |
Author | Edward T. Curran |
Publisher | |
Pages | 17 |
Release | 1974 |
Genre | |
ISBN |
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 Ramjets
Title | Integral Rocket Ramjets PDF eBook |
Author | R. F. Calzone |
Publisher | |
Pages | 49 |
Release | 1994 |
Genre | |
ISBN |
A rough overview of the important aspects and problem areas associated with the development of Integral Rocket Ramjet (IRR) technology is given in this report. The IRR is a supersonic air-breathing concept in which the gas generator produces fuel-rich gases. These fuel-rich gases are burnt in the secondary combustion chamber with ambient air captured and decelerated in the inlet. During the boost phase, a solid propellant booster provides the thrust necessary to achieve the velocity at which the ramjet may be operated (about M = 2). The booster is integrated in the secondary combustion chamber.
A Unified Analysis of Ramjet Operation in an Integrated Rocket Ramjet Engine Part 1. Transition from Rocket Booster to Ramject Sustainer
Title | A Unified Analysis of Ramjet Operation in an Integrated Rocket Ramjet Engine Part 1. Transition from Rocket Booster to Ramject Sustainer PDF eBook |
Author | Hong-Gye Sung |
Publisher | |
Pages | |
Release | 2001 |
Genre | |
ISBN |