Add to ORKGAerodynamic data obtained from wind tunnel tests of an 0.015-scale space shuttle vehicle Orbiter model of a 140A/B configuration with modified orbital manuevering system pods and elevons are documented. Force data was obtained at various control surface settings and Reynolds numbers in the angle of attack range of 15 deg to 45 deg and at angles of sideslip of -5 deg to +5 deg. Control surface variables included elevon, rudder, speed brake, and body flap configurations
The results of wind tunnel tests of the 140A/B configuration components are reported for the fuselag...
Experimental aerodynamic investigations were conducted on a 0.015 scale model of the Space Shuttle O...
Tests were conducted in wind tunnels during April and May 1973, on a 0.030-scale replica of the Spac...
Aerodynamic data obtained from wind tunnel tests of an 0.015-scale 140A/B configuration SSV Orbiter ...
Data obtained from a wind tunnel test of an 0.015-scale 140 A/B configuration space shuttle vehicle ...
Experimental aerodynamic investigations were conducted on a scale model of the space shuttle orbiter...
A wind tunnel test of an 0.030-scale space shuttle vehicle orbiter configuration 140A/B model was co...
These tests were conducted to obtain longitudinal stability and control data for Mach numbers from 0...
Data obtained from a wind tunnel test of a 0.015-scale 140A/B configuration SSV orbiter model are pr...
Experimental aerodynamic investigations were conducted in the NASA/Ames 3.5-Foot Hypersonic wind Tun...
Tests were conducted in the NASA/ARC Unitary Plan wind tunnels on an 0.030-scale replica of the spac...
Aerodynamic force and moment tests were conducted on an 0.015-scale space shuttle vehicle configurat...
Longitudinal and lateral-directional stability and control characteristics were evaluated at Mach nu...
A wind tunnel test was conducted of an 0.030 scale model of the space shuttle orbiter in a supersoni...
Wind tunnel tests were conducted of the NASA/Rockwell 0.015 scale configuration 4 mated space shuttl...
The results of wind tunnel tests of the 140A/B configuration components are reported for the fuselag...
Experimental aerodynamic investigations were conducted on a 0.015 scale model of the Space Shuttle O...
Tests were conducted in wind tunnels during April and May 1973, on a 0.030-scale replica of the Spac...
Aerodynamic data obtained from wind tunnel tests of an 0.015-scale 140A/B configuration SSV Orbiter ...
Data obtained from a wind tunnel test of an 0.015-scale 140 A/B configuration space shuttle vehicle ...
Experimental aerodynamic investigations were conducted on a scale model of the space shuttle orbiter...
A wind tunnel test of an 0.030-scale space shuttle vehicle orbiter configuration 140A/B model was co...
These tests were conducted to obtain longitudinal stability and control data for Mach numbers from 0...
Data obtained from a wind tunnel test of a 0.015-scale 140A/B configuration SSV orbiter model are pr...
Experimental aerodynamic investigations were conducted in the NASA/Ames 3.5-Foot Hypersonic wind Tun...
Tests were conducted in the NASA/ARC Unitary Plan wind tunnels on an 0.030-scale replica of the spac...
Aerodynamic force and moment tests were conducted on an 0.015-scale space shuttle vehicle configurat...
Longitudinal and lateral-directional stability and control characteristics were evaluated at Mach nu...
A wind tunnel test was conducted of an 0.030 scale model of the space shuttle orbiter in a supersoni...
Wind tunnel tests were conducted of the NASA/Rockwell 0.015 scale configuration 4 mated space shuttl...
The results of wind tunnel tests of the 140A/B configuration components are reported for the fuselag...
Experimental aerodynamic investigations were conducted on a 0.015 scale model of the Space Shuttle O...
Tests were conducted in wind tunnels during April and May 1973, on a 0.030-scale replica of the Spac...