DESIGN OF A N~20/HTPB HYBRID ROCKET MOTOR UTILIZING A TOROIDAL AEROSPIKE NOZZLE
DESIGN OF A N~20/HTPB HYBRID ROCKET MOTOR UTILIZING A TOROIDAL AEROSPIKE NOZZLE
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Document information
DESIGN OF A N~20/HTPB HYBRID ROCKET MOTOR UTILIZING A TOROIDAL AEROSPIKE NOZZLE
48th, Aerospace sciences meeting; 48th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition ; 2010 ; Orlando, FL
2010-01-01
11 pages
Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009
Conference paper
English
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