Space Shuttle External Tank Instrumentation Evaluation.
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFS TN
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Data were obtained on the performance of space shuttle flight instrumentation under simulated flight conditions. These conditions included ablating insulation material. The tests were conducted at a free-stream Mach number of 10 and tunnel stilling chamber conditions of 1800 psia and 1900 R. Author
- Unmanned Spacecraft
- Spacecraft Trajectories and Reentry