Design And Evaluation Of A Turbojet Exhaust Simulator, Utilizing A Solid-propellant Rocket Motor, For Use In Free-flight Aerodynam

by Nasa Technical Reports Server (ntrs)

2021-01-11 10:47:47

A method has been developed for modifying a rocket motor so that its exhaust characteristics simulate those of a turbojet engine. The analysis necessary to the design is presented along with tests from which the designs are evaluated. Simulation was ... Read more
A method has been developed for modifying a rocket motor so that its exhaust characteristics simulate those of a turbojet engine. The analysis necessary to the design is presented along with tests from which the designs are evaluated. Simulation was found to be best if the exhaust characteristics to be duplicated were those of a turbojet engine at high altitudes and with the afterburner operative. Less

Book Details

File size9.69 X 7.44 X 0.06 in
Print pages30
PublisherBiblioGov
Publication date July 31, 2013
LanguageEnglish
ISBN9781289264192

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