Add to ORKGDesign, fabrication and static testing of attached inflatable decelerator models for supersonic wind tunnel evaluatio
The supersonic aerodynamic and aeroelastic characteristics of a tension cone inflatable aerodynamic ...
Mach 8 variable-density tunnel used for determination of aerodynamic heating of attached inflatable ...
Aerodynamic characteristics of inflatable structure paraglider tested in wind tunne
Design, fabrication, and static testing of wind tunnel models of first-stage Attached Inflatable Dec...
The testing of 3- and 6-meter diameter Hypersonic Inflatable Aerodynamic Decelerator (HIAD) test art...
Inflatable conical shell afterbody ballute for aerodynamic brakes in Mars atmospheric entr
Meridional tape forces, permeability, and change in model contours were measured on the aft half of ...
Trajectory, thermodynamic, and stress analyses of spacecraft inflatable decelerators in Mars and Ear...
Attached-inflatable-decelerator (AID) canopies fabricated from lightweight Nomex cloth and tapes wer...
Acceptance of new spacecraft structural architectures and concepts requires validated design methods...
Deployment and performance characteristics of 5-Foot diameter (1.5m) Attached Inflatable Decelerator...
Experimental design of deployable tension cone decelerator with inflatable toroids for compression r...
The current limits of supersonic parachute technology may constrain the ability to safely land futur...
Since the 1970's, NASA has relied on the use of rigid aeroshells and supersonic parachutes to enable...
A wind-tunnel investigation was conducted at free-stream Mach numbers from 0.20 to 1.00 and correspo...
The supersonic aerodynamic and aeroelastic characteristics of a tension cone inflatable aerodynamic ...
Mach 8 variable-density tunnel used for determination of aerodynamic heating of attached inflatable ...
Aerodynamic characteristics of inflatable structure paraglider tested in wind tunne
Design, fabrication, and static testing of wind tunnel models of first-stage Attached Inflatable Dec...
The testing of 3- and 6-meter diameter Hypersonic Inflatable Aerodynamic Decelerator (HIAD) test art...
Inflatable conical shell afterbody ballute for aerodynamic brakes in Mars atmospheric entr
Meridional tape forces, permeability, and change in model contours were measured on the aft half of ...
Trajectory, thermodynamic, and stress analyses of spacecraft inflatable decelerators in Mars and Ear...
Attached-inflatable-decelerator (AID) canopies fabricated from lightweight Nomex cloth and tapes wer...
Acceptance of new spacecraft structural architectures and concepts requires validated design methods...
Deployment and performance characteristics of 5-Foot diameter (1.5m) Attached Inflatable Decelerator...
Experimental design of deployable tension cone decelerator with inflatable toroids for compression r...
The current limits of supersonic parachute technology may constrain the ability to safely land futur...
Since the 1970's, NASA has relied on the use of rigid aeroshells and supersonic parachutes to enable...
A wind-tunnel investigation was conducted at free-stream Mach numbers from 0.20 to 1.00 and correspo...
The supersonic aerodynamic and aeroelastic characteristics of a tension cone inflatable aerodynamic ...
Mach 8 variable-density tunnel used for determination of aerodynamic heating of attached inflatable ...
Aerodynamic characteristics of inflatable structure paraglider tested in wind tunne