VOLUME 2 OF 2 TRIPLE BALANCE TEST OF THE PRR BASELINE SPACE SHUTTLE CONFIGURATION ON A .004 SCALE MODEL OF THE MCR 0074 ORBITER CONFIGURATION IN THE MSFC 14 × 14 INCH TRISONIC WIND TUNNEL (TWT 570) [IA31F(B)]

摘要

In addition to the static stability data, other runs were made to identify key simulation parameters to be used in future launch vehicle wind tunnel tests. The following parameters were investigated:nEffect of Orbiter - ET attach hardwarenModel attachment (spacer) effectsnEffects of "grit" on model leading surfacesnModel misalignment effects