Final report on fundamental phenomena on fuel decomposition and boundary-layer combustion precesses with applications to hybrid rocket motors

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Penn State, National Aeronautics and Space Administration, National Technical Information Service, distributor , University Park, Pa, [Washington, D.C, Springfield, Va
Hybrid rocket engines., Propulsion system performance., Ducted rocket engines., Combustion physics., Boundary layers., Fuel combus
Other titlesFundamental phenomena on fuel decomposition and boundary-layer combustion precesses with applications to hybrid rocket motors.
Statementprepared by part I: Kenneth K. Kuo ... [et al.]; part II: Charles L. Merkle and Sankaran Venkateswaran.
Series[NASA contractor report] -- NASA-CR-201843., NASA contractor report -- NASA CR-201843.
ContributionsKuo, Kenneth K., Merkle, C. L., Venkateswaran, Sankaran., United States. National Aeronautics and Space Administration.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL15499034M