Publication Date:
2019-07-11
Description:
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.
Keywords:
Aircraft Propulsion and Power
Type:
NACA-RM-L54I15
Format:
application/pdf
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