Wind tunnel test results from shuttle solid rocket booster (SRB) sting interference tests were evaluated, yielding the general influence of the sting on the normal force and pitching moment coefficients and the side force and yawing moment coefficients. The procedures developed to determine the sting interference, the development of the corrected aerodynamic data, and the development of a new SRB aerodynamic mathematical model are documented.
Space Shuttle Solid Rocket Booster Sting Interference Wind Tunnel Test Analysis
1981
235 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Rocket Engines & Motors , Space shuttle boosters , Support interference , Wind tunnel apparatus , Wind tunnel models , Wind tunnel tests , Aerodynamic coefficients , Angle of attack , Axial loads , Data bases , Mathematical models , Pitching moments , Reynolds number , Rolling moments , Spacecraft configurations , Structural influence coefficients , Trisonic wind tunnels
Space Shuttle solid rocket booster
NTRS | 1979
|Space Shuttle system solid rocket booster.
NTRS | 1973
|Space Shuttle system solid rocket booster
AIAA | 1973
|