The objective of the program was to demonstrate the applicability of the Holloman test track for performing captive tests of a ramjet engine at realistic supersonic flight conditions and to provide sled design data for future sled-borne aero propulsion systems. This objective was achieved by designing a series of four track test systems to increasingly higher performance levels, the fourth of which culminated in propelling a structurally sound flight test missile payload to a sustained velocity in excess of 2600 ft/sec for 3.6 seconds. The velocity profile is sufficient to proceed with ignition and testing of the payload ramjet engine. (Author)
Environmental Investigation of Pilot Propulsion Test Sled
1974
198 pages
Report
Keine Angabe
Englisch
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