Airloads investigation of an 0.030 scale model of the space shuttle vehicle 140A/B orbiter configuration (model 47-0) in the arc 9 by 7-foot unitary plan wind tunnel for Mach 1.55 and 2.2 (OA22B)
Abstract
For abstract, see N75-23647.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- April 1975
- Bibcode:
- 1975STIN...7523650G
- Keywords:
-
- Launch Vehicle Configurations;
- Space Shuttle Orbiters;
- Wind Tunnel Models;
- Wind Tunnel Tests;
- Aerodynamic Loads;
- Angle Of Attack;
- Pressure Distribution;
- Sideslip;
- Space Shuttle Boosters;
- Supersonic Speed;
- Wing Tanks;
- Launch Vehicles and Space Vehicles