An analytical study of mode transition in the integral ramjet-rocket class of propulsion system was conducted. A baseline design was selected and used for analysis. The several factors affecting the engine aerothermodynamic performance during mode transition were evaluated. A quantitative evaluation method was established to aid in design of future engines of this class. Specific developmental recommendations are made. (Author)
Mode Transition in Integral Ramjet Rocket Propulsion Systems
1972
65 pages
Report
Keine Angabe
Englisch
Combustion & Ignition , Supersonic combustion , Hybrid rockets , Supersonic combustion ramjet engines , Reaction kinetics , Rocket motors(Solid propellant) , Rocket propellant grains , Diffusers , Ramjet engine nozzles , Configuration , Nozzle inserts , Specific impulse , Burning rate , Ramjet rocket propulsion system , Transition process
Propulsion System Analysis and Flight Test of an Integral Rocket Ramjet
British Library Conference Proceedings | 1995
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