Publication Date:
2019-06-27
Description:
Longitudinal and lateral-directional stability and control characteristics were evaluated at Mach numbers of 5.3, 7.3 and 10.3 at angles of attack up to 50 degrees with Beta = 0 degrees and, for a few cases, Beta = 5 degrees. Component force data, fuselage base pressures and shadowgraph patterns were recorded.
Keywords:
SPACE VEHICLES
Type:
NASA-CR-128799
,
DMS-DR-2071
Format:
application/pdf