Add to ORKGTabulated pressure data are presented on the left upper wing surface of the integrated space shuttle vehicle configuration. For Vol. 1, see N76-15246
Tests were conducted in wind tunnels during April and May 1973, on a 0.030-scale replica of the Spac...
The primary objective of the test was to obtain stability and control data for the basic configurati...
The results of a wind tunnel test to determine the force, moment, and hinge-moment characteristics o...
Tabulated pressure data are presented on the left lower wing surface of a scale model of the integra...
Tabulated pressure data are presented on the orbiter fuselage and left vertical tail surface of a sc...
Results of wind tunnel tests on a 0.030-scale model of the integrated space shuttle vehicle configur...
Tabulated force data and plotted pressure data are presented on a scale model of the integrated spac...
Tabulated pressure data are presented on the right upper wing surface, right lower wing surface, and...
Tests were conducted in the NASA/ARC Unitary Plan wind tunnels on an 0.030-scale replica of the spac...
Experimental aerodynamic investigations were conducted on a scale model of the space shuttle orbiter...
Experimental aerodynamic investigations were conducted on an 0.0405 scale representation of the Rock...
Tests were conducted in wind tunnels during April and May 1973, on a 0.030-scale replica of the Spac...
The results of wind tunnel tests conducted on a 0.010-scale version of the Vehicle 3 Space Shuttle C...
The investigations of pressure distributions are presented for aeroloads analysis at Mach numbers fr...
Two prototype solar heating systems, consisting of the following subsystems: collector, control, an...
Tests were conducted in wind tunnels during April and May 1973, on a 0.030-scale replica of the Spac...
The primary objective of the test was to obtain stability and control data for the basic configurati...
The results of a wind tunnel test to determine the force, moment, and hinge-moment characteristics o...
Tabulated pressure data are presented on the left lower wing surface of a scale model of the integra...
Tabulated pressure data are presented on the orbiter fuselage and left vertical tail surface of a sc...
Results of wind tunnel tests on a 0.030-scale model of the integrated space shuttle vehicle configur...
Tabulated force data and plotted pressure data are presented on a scale model of the integrated spac...
Tabulated pressure data are presented on the right upper wing surface, right lower wing surface, and...
Tests were conducted in the NASA/ARC Unitary Plan wind tunnels on an 0.030-scale replica of the spac...
Experimental aerodynamic investigations were conducted on a scale model of the space shuttle orbiter...
Experimental aerodynamic investigations were conducted on an 0.0405 scale representation of the Rock...
Tests were conducted in wind tunnels during April and May 1973, on a 0.030-scale replica of the Spac...
The results of wind tunnel tests conducted on a 0.010-scale version of the Vehicle 3 Space Shuttle C...
The investigations of pressure distributions are presented for aeroloads analysis at Mach numbers fr...
Two prototype solar heating systems, consisting of the following subsystems: collector, control, an...
Tests were conducted in wind tunnels during April and May 1973, on a 0.030-scale replica of the Spac...
The primary objective of the test was to obtain stability and control data for the basic configurati...
The results of a wind tunnel test to determine the force, moment, and hinge-moment characteristics o...