The purpose of this report is to present a test plan for thermodynamic heat transfer and pressure tests of a 9-percent Gemini B model in the hypervelocity impulse tunnel. The model will have interchangeable re-entry module-adapter interconnect fairings which will simulate the NASA Gemini and Gemini B configurations. (Author)
Test Plan for Aerodynamic Heating and Pressure Tests of a 9-Percent Gemini B Re-Entry Configuration Model in the McDonnell Hypervelocity Impulse Tunnel
1967
31 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Manned spacecraft , Space stations , Reentry vehicles , Atmosphere entry , Hypersonic test vehicles , Hypersonic characteristics , Models(Simulations) , Configuration , Hypersonic wind tunnels , Flared afterbodies , Angle of attack , Fairings , Thermodynamics , Gemini b project , Manned orbiting laboratories , Mol(Manned orbiting laboratories) , Thermographic mapping
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