Add to ORKGIn-flight dynamic simulator used to evaluate problems of low-speed approach and landing of supersonic transpor
Cruise scene visual attachment system assembly and detail design drawings for manned spacecraft or a...
The trajectory data presented are to be used for orbiter systems and subsystems evalation, flight an...
Tests were conducted in the NASA/ARC Unitary Plan Wind Tunnels on an 0.030 scale replica of the spac...
Four-engine jet aircraft used as in-flight simulator for variable stability testing of supersonic ai...
Comparison of theoretical and simulated low speed landing characteristics for large transport aircra...
A nondimensional economic examination of a parametrically-derived set of supersonic transport aircra...
Aerodynamic investigations were conducted in a low speed wind tunnel from June 18 through June 25, 1...
The definition of standard flight segments of phases, representing flight profile components which c...
Performance data are presented for the tunnel, which has a Mach number range from 0.36 to 2.0. The t...
The papers in this compilation were presented at the NASA Symposium on "Supercritical Wing Technolog...
Preliminary data are documented for a typical launch window opening, a typical in-plane case, and a ...
Static tests of augmentor-wing flap system for modified C-8A jet STOL research airplane using 0.7 sc...
Experimental investigations were performed in a 6- by 6-Foot Supersonic wind tunnel on a 0.015-scale...
Wind tunnel tests were conducted of the NASA/Rockwell 0.015 scale configuration 4 mated space shuttl...
When asked by the Aeronautical Engineering staff to design a viable supersonic commercial transport,...
Cruise scene visual attachment system assembly and detail design drawings for manned spacecraft or a...
The trajectory data presented are to be used for orbiter systems and subsystems evalation, flight an...
Tests were conducted in the NASA/ARC Unitary Plan Wind Tunnels on an 0.030 scale replica of the spac...
Four-engine jet aircraft used as in-flight simulator for variable stability testing of supersonic ai...
Comparison of theoretical and simulated low speed landing characteristics for large transport aircra...
A nondimensional economic examination of a parametrically-derived set of supersonic transport aircra...
Aerodynamic investigations were conducted in a low speed wind tunnel from June 18 through June 25, 1...
The definition of standard flight segments of phases, representing flight profile components which c...
Performance data are presented for the tunnel, which has a Mach number range from 0.36 to 2.0. The t...
The papers in this compilation were presented at the NASA Symposium on "Supercritical Wing Technolog...
Preliminary data are documented for a typical launch window opening, a typical in-plane case, and a ...
Static tests of augmentor-wing flap system for modified C-8A jet STOL research airplane using 0.7 sc...
Experimental investigations were performed in a 6- by 6-Foot Supersonic wind tunnel on a 0.015-scale...
Wind tunnel tests were conducted of the NASA/Rockwell 0.015 scale configuration 4 mated space shuttl...
When asked by the Aeronautical Engineering staff to design a viable supersonic commercial transport,...
Cruise scene visual attachment system assembly and detail design drawings for manned spacecraft or a...
The trajectory data presented are to be used for orbiter systems and subsystems evalation, flight an...
Tests were conducted in the NASA/ARC Unitary Plan Wind Tunnels on an 0.030 scale replica of the spac...