Space Shuttle orbiter trimmed center-of-gravity extension study
Abstract
Aerodynamic, heat transfer, and system design studies to determine removable modifications for the Space Shuttle orbiter that would extend its forward center-of-gravity triom capability are summarized. Wind-tunnel tests were conducted at Mach numbers ranging from 0.25 to 20.3 to determine the most effective aerodynamic modifications. Heat transfer and system design studies determined the impact of the modifications on the thermal protection system and structural weight of the vehicle. The most effective modifications were in-fillet canards or a forward extension of the existing forward wing fillet.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- March 1985
- Bibcode:
- 1985STIN...8519003S
- Keywords:
-
- Aerodynamic Configurations;
- Canard Configurations;
- Center Of Gravity;
- Space Shuttle Orbiters;
- Aerodynamic Heating;
- Design Analysis;
- Fillets;
- Heat Transfer;
- Retrofitting;
- Thermal Protection;
- Wind Tunnel Tests;
- Launch Vehicles and Space Vehicles