Data tables, model figures, and tabulated source data are given for aerodynamic investigations of separation effects in the integrated space shuttle vehicle. For Volume 1, see N75-28101.
Aerodynamic Results of a Separation Effects Test (IA87) on a 0.01-Scale Model (52-Ots) of the Integrated Ssv in the AEDC/Vkf 40-by-40 Inch Supersonic Wind Tunnel a, Volume 2
1975
583 pages
Report
Keine Angabe
Englisch