Longitudinal Aerodynamic Characteristics of Ten Booster-Glider Models for Project Dyna-Soar at Mach Numbers of 0.7 and 1.0.

摘要

A wind-tunnel investigation has been made of ten hypersonic booster-glider models at Mach numbers of 0-7 and 1.0. Only the booster portions of the model configurations were varied. Lift, drag, pitching-moment, and base-pressure data were obtained for a maximum angle-of-attack range of -10 to 11 deg. These data have not been analyzed since it was desired to expedite the publication of the results.