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The Pulse Detonation Rocket Induced MHD Ejector (PDRIME) Concept (Preprint) 5b. GRANT NUMBER
The Pulse Detonation Rocket Induced MHD Ejector (PDRIME) Concept (Preprint) 5b. GRANT NUMBER
2008
E. Saturn Blvd
Edwards Afb
Keywords:
Magnetohydrodynamics
Aeronautics
Preprint
Injector
Rocket
Aerospace engineering
Pulse (signal processing)
Detonation
Engineering
Correction
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