Publication Date:
2019-06-27
Description:
An experimental test program has been conducted to measure the dynamic stability derivatives of a modified 089B shuttle orbiter. Subsonic and transonic forced oscillation tests were conducted in the Langley 8 foot TPT tunnel over a Mach number range from 0.3 to 1.2 for angles of attack up to 22 deg. The data were measured at the model resonant frequency with pitch and yaw amplitudes of 1 deg and a roll amplitude of 2.5 deg.
Keywords:
SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Type:
NASA-TM-X-72631
Format:
application/pdf
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