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Aerodynamic investigations were conducted in a low speed wind tunnel from June 18 through June 25, 1973 on a 0.0405 scale -139B model Space Shuttle Vehicle orbiter. The purpose of the test was to investigate the longitudinal and lateral-directional subsonic aerodynamic characteristics of the proposed PRR Space Shuttle Orbiter. Emphasis was placed on component buildup effects, elevon, rudder, body flaps, rudder flare effectiveness, and canard and speed brake development. Angles of attack from -4 to 24 and angles of sideslip of -10 to 10 were tested. Static pressures were recorded on the base. The aerodynamic force balance results are presented in plotted and tabular form
Wind tunnel tests were conducted of the NASA/Rockwell 0.015 scale configuration 4 mated space shuttl...
Experimental aerodynamic investigations were conducted on 0.015 scale representations of two Space S...
Experimental aerodynamic investigations were conducted in the NASA/Ames 3.5-Foot Hypersonic wind Tun...
Experimental aerodynamic investigations were conducted in a low speed wind tunnel from May 21 throug...
Experimental investigations were performed in a 6- by 6-Foot Supersonic wind tunnel on a 0.015-scale...
Tests were conducted in wind tunnels during April and May 1973, on a 0.030-scale replica of the Spac...
Tests were conducted in the NASA/ARC Unitary Plan Wind Tunnels on an 0.030 scale replica of the spac...
Tests were conducted in the NASA/ARC Unitary Plan wind tunnels on an 0.030-scale replica of the spac...
A wind tunnel test was conducted of an 0.030 scale model of the space shuttle orbiter in a supersoni...
Tests were conducted in unitary plan wind tunnels on an 0.030-scale replica of the space shuttle veh...
Tests were conducted in wind tunnels during April and May 1973, on an 0.030-scale replica of the Spa...
A wind tunnel test of an 0.030-scale space shuttle vehicle orbiter configuration 140A/B model was co...
Data obtained from a wind tunnel test of an 0.015-scale 140 A/B configuration space shuttle vehicle ...
The results of a wind tunnel test to determine the force, moment, and hinge-moment characteristics o...
Experimental aerodynamic investigations were conducted on a scale model of the space shuttle orbiter...
Wind tunnel tests were conducted of the NASA/Rockwell 0.015 scale configuration 4 mated space shuttl...
Experimental aerodynamic investigations were conducted on 0.015 scale representations of two Space S...
Experimental aerodynamic investigations were conducted in the NASA/Ames 3.5-Foot Hypersonic wind Tun...
Experimental aerodynamic investigations were conducted in a low speed wind tunnel from May 21 throug...
Experimental investigations were performed in a 6- by 6-Foot Supersonic wind tunnel on a 0.015-scale...
Tests were conducted in wind tunnels during April and May 1973, on a 0.030-scale replica of the Spac...
Tests were conducted in the NASA/ARC Unitary Plan Wind Tunnels on an 0.030 scale replica of the spac...
Tests were conducted in the NASA/ARC Unitary Plan wind tunnels on an 0.030-scale replica of the spac...
A wind tunnel test was conducted of an 0.030 scale model of the space shuttle orbiter in a supersoni...
Tests were conducted in unitary plan wind tunnels on an 0.030-scale replica of the space shuttle veh...
Tests were conducted in wind tunnels during April and May 1973, on an 0.030-scale replica of the Spa...
A wind tunnel test of an 0.030-scale space shuttle vehicle orbiter configuration 140A/B model was co...
Data obtained from a wind tunnel test of an 0.015-scale 140 A/B configuration space shuttle vehicle ...
The results of a wind tunnel test to determine the force, moment, and hinge-moment characteristics o...
Experimental aerodynamic investigations were conducted on a scale model of the space shuttle orbiter...
Wind tunnel tests were conducted of the NASA/Rockwell 0.015 scale configuration 4 mated space shuttl...
Experimental aerodynamic investigations were conducted on 0.015 scale representations of two Space S...
Experimental aerodynamic investigations were conducted in the NASA/Ames 3.5-Foot Hypersonic wind Tun...
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