A force test of a scale model of the Space Shuttle Solid Rocket Booster was conducted in a trisonic wind tunnel. The model was tested with such protuberances as a camera capsule, electrical tunnel, attach rings, aft separation rockets, ET attachment structure, and hold-down struts. The model was also tested with the nozzle at gimbal angles of 0, 2.5, and 5 degrees. The influence of a unique heat shield configuration was also determined. Some photographs of model installations in the tunnel were taken and are included. Schlieren photography was utilized for several angles of attack
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
Aero-loads investigations were conducted on the updated configuration-5 space shuttle launch vehicle...
The results of the tests are presented along with aerodynamic loads data obtained at Mach numbers fr...
The results of a pressure test of a .00548 scale 146 inch Space Shuttle Solid Rocket Booster (SRB) w...
A force test of a 2.112 percent scale Space Shuttle Solid Rocket Booster (SRB), MSFC Model 454, was ...
Force tests of a 0.563 percent scale space shuttle solid rocket booster (SRB) model, MSFC Model 449,...
An experimental investigation was conducted in the MSFC 14 inch TWT to study the roll characteristic...
An experimental investigation (SA16F) was conducted in the AEDC PWT 4T to determine the entry static...
Tests of a 2.112 percent scale model of the space shuttle solid rocket booster model were conducted ...
A test of a 0.563 percent scale space shuttle Solid Rocket Booster (SRB) model, MSFC Model 449, was ...
An experimental investigation (SA14FA, TWT 620) was conducted in the MSFC 14-inch Trisonic Wind Tunn...
Experimental aerodynamic investigations were made in the Grumman 36-inch hypersonic wind tunnel on a...
Static pressure distributions for the external tank (ET) at reentry conditions are presented. Basic ...
Results of tests conducted on an 0.030-scale launch configuration model of the space shuttle vehicle...
An experimental Aerodynamic and Aero-Acoustic loads data base was obtained at transonic Mach numbers...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
Aero-loads investigations were conducted on the updated configuration-5 space shuttle launch vehicle...
The results of the tests are presented along with aerodynamic loads data obtained at Mach numbers fr...
The results of a pressure test of a .00548 scale 146 inch Space Shuttle Solid Rocket Booster (SRB) w...
A force test of a 2.112 percent scale Space Shuttle Solid Rocket Booster (SRB), MSFC Model 454, was ...
Force tests of a 0.563 percent scale space shuttle solid rocket booster (SRB) model, MSFC Model 449,...
An experimental investigation was conducted in the MSFC 14 inch TWT to study the roll characteristic...
An experimental investigation (SA16F) was conducted in the AEDC PWT 4T to determine the entry static...
Tests of a 2.112 percent scale model of the space shuttle solid rocket booster model were conducted ...
A test of a 0.563 percent scale space shuttle Solid Rocket Booster (SRB) model, MSFC Model 449, was ...
An experimental investigation (SA14FA, TWT 620) was conducted in the MSFC 14-inch Trisonic Wind Tunn...
Experimental aerodynamic investigations were made in the Grumman 36-inch hypersonic wind tunnel on a...
Static pressure distributions for the external tank (ET) at reentry conditions are presented. Basic ...
Results of tests conducted on an 0.030-scale launch configuration model of the space shuttle vehicle...
An experimental Aerodynamic and Aero-Acoustic loads data base was obtained at transonic Mach numbers...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
Aero-loads investigations were conducted on the updated configuration-5 space shuttle launch vehicle...
The results of the tests are presented along with aerodynamic loads data obtained at Mach numbers fr...