Design of a N20/HTPB Hybrid Rocket Motor Utilizing a Toroidal Aerospike Nozzle
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
01.01.2010
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
DESIGN OF A N~20/HTPB HYBRID ROCKET MOTOR UTILIZING A TOROIDAL AEROSPIKE NOZZLE
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