Topics
NASACompany
The successful flight of the Inflatable Reentry Vehicle Experiment (IRVE)-3 has further demonstrated the potential value of Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology. This technology development effort is funded by NASA's Space Technology Mission Directorate (STMD) Game Changing Development Program (GCDP). This paper provides an overview of a multi-year HIAD technology development effort, detailing the projects completed to date and the additional testing planned for the future
NASA's Low Density Supersonic Decelerator (LDSD) program was established to identify, develop, and e...
Inflatable aeroshells offer several advantages over traditional rigid aeroshells for atmospheric ent...
Acceptance of new spacecraft structural architectures and concepts requires validated design methods...
Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology readiness levels have been increment...
The testing of 3- and 6-meter diameter Hypersonic Inflatable Aerodynamic Decelerator (HIAD) test art...
This paper describes a proposed orbital velocity reentry flight test of a Hypersonic Inflatable Aero...
The Inflatable Reentry Vehicle Experiment 3 (IRVE-3) launched July 23, 2012, from NASA Wallops Fligh...
To support NASAs long term goal of landing humans on Mars, technologies which enable the landing of ...
Supersonic inflatable aerodynamic decelerators (IADs) are drag devices intended to be deployed at hi...
Supersonic inflatable aerodynamic decelerators (IADs) are drag devices intended to be deployed at hi...
NASAs Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology was selected for a Technology ...
Since the 1970's, NASA has relied on the use of rigid aeroshells and supersonic parachutes to enable...
Over a decade of work has been conducted in the development of NASAs Hypersonic Inflatable Aerodynam...
This presentation was part of the session : Cross Cutting TechnologiesSixth International Planetary ...
To support NASAs long term goal of landing humans on Mars, technologies which enable the landing of ...
NASA's Low Density Supersonic Decelerator (LDSD) program was established to identify, develop, and e...
Inflatable aeroshells offer several advantages over traditional rigid aeroshells for atmospheric ent...
Acceptance of new spacecraft structural architectures and concepts requires validated design methods...
Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology readiness levels have been increment...
The testing of 3- and 6-meter diameter Hypersonic Inflatable Aerodynamic Decelerator (HIAD) test art...
This paper describes a proposed orbital velocity reentry flight test of a Hypersonic Inflatable Aero...
The Inflatable Reentry Vehicle Experiment 3 (IRVE-3) launched July 23, 2012, from NASA Wallops Fligh...
To support NASAs long term goal of landing humans on Mars, technologies which enable the landing of ...
Supersonic inflatable aerodynamic decelerators (IADs) are drag devices intended to be deployed at hi...
Supersonic inflatable aerodynamic decelerators (IADs) are drag devices intended to be deployed at hi...
NASAs Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology was selected for a Technology ...
Since the 1970's, NASA has relied on the use of rigid aeroshells and supersonic parachutes to enable...
Over a decade of work has been conducted in the development of NASAs Hypersonic Inflatable Aerodynam...
This presentation was part of the session : Cross Cutting TechnologiesSixth International Planetary ...
To support NASAs long term goal of landing humans on Mars, technologies which enable the landing of ...
NASA's Low Density Supersonic Decelerator (LDSD) program was established to identify, develop, and e...
Inflatable aeroshells offer several advantages over traditional rigid aeroshells for atmospheric ent...
Acceptance of new spacecraft structural architectures and concepts requires validated design methods...
Add to ORKG