Add to ORKGStress analysis and friction coefficient determination for expandable tube type shock absorbe
Flight test and evaluative data relating to design and use of elastomeric shield materials for therm...
The design, development, construction, and testing of the Long Duration Exposure Facility inflatable...
Design, fabrication and static testing of attached inflatable decelerator models for supersonic wind...
Design, fabrication, and static testing of wind tunnel models of first-stage Attached Inflatable Dec...
Boundary layer blowing techniques for high lift stator blades in axial flow compressor
Aerodynamic, structural, and thermal analyses for supersonic planetary entry parachute desig
The testing of 3- and 6-meter diameter Hypersonic Inflatable Aerodynamic Decelerator (HIAD) test art...
Trajectory, thermodynamic, and stress analyses of spacecraft inflatable decelerators in Mars and Ear...
A parachute fabric for aerodynamic decelerator applications is described. The fabric will permit dep...
Structural model to evaluate evacuated multiwall structure for hypersonic aircraf
Mach 8 variable-density tunnel used for determination of aerodynamic heating of attached inflatable ...
Attached-inflatable-decelerator (AID) canopies fabricated from lightweight Nomex cloth and tapes wer...
Experimental design of deployable tension cone decelerator with inflatable toroids for compression r...
Report includes the National Advisory Committee for Aeronautics letter of submittal to the President...
Stress analysis and friction coefficient determination for expandable tube type shock absorbe
Flight test and evaluative data relating to design and use of elastomeric shield materials for therm...
The design, development, construction, and testing of the Long Duration Exposure Facility inflatable...
Design, fabrication and static testing of attached inflatable decelerator models for supersonic wind...
Design, fabrication, and static testing of wind tunnel models of first-stage Attached Inflatable Dec...
Boundary layer blowing techniques for high lift stator blades in axial flow compressor
Aerodynamic, structural, and thermal analyses for supersonic planetary entry parachute desig
The testing of 3- and 6-meter diameter Hypersonic Inflatable Aerodynamic Decelerator (HIAD) test art...
Trajectory, thermodynamic, and stress analyses of spacecraft inflatable decelerators in Mars and Ear...
A parachute fabric for aerodynamic decelerator applications is described. The fabric will permit dep...
Structural model to evaluate evacuated multiwall structure for hypersonic aircraf
Mach 8 variable-density tunnel used for determination of aerodynamic heating of attached inflatable ...
Attached-inflatable-decelerator (AID) canopies fabricated from lightweight Nomex cloth and tapes wer...
Experimental design of deployable tension cone decelerator with inflatable toroids for compression r...
Report includes the National Advisory Committee for Aeronautics letter of submittal to the President...
Stress analysis and friction coefficient determination for expandable tube type shock absorbe
Flight test and evaluative data relating to design and use of elastomeric shield materials for therm...
The design, development, construction, and testing of the Long Duration Exposure Facility inflatable...