NASA's ASPIRE (Advanced Supersonic Parachute Inflation ResearchExperiments) project is investigating the supersonic deployment, inflation andaerodynamics of full-scale disk-gap-band (DGB) parachutes. The first two flight tests werecarried out in October 2017 and March 2018, while a third test is planned for the fall of 2018. Inthese tests, Mars-relevant conditions are achieved by deploying the parachutes at high altitudesover Earth using a sounding rocket test platform. As a result, the parachute is deployed behind aslender body (roughly 1/6-th the diameter of the capsule that will use this parachute for descentat Mars). Because there is limited flight and experimental data for supersonic DGBs behindslender bodies, the development of the pa...
Inflation and drag characteristics of cross parachute in simulated Martian environmen
The Low Density Supersonic Decelerator Project is developing a next-generation supersonic parachute ...
Models are presented for the aerodynamic coefficients of Supersonic Ringsail and Disk-Gap-Band parac...
NASAs ASPIRE (Advanced Supersonic Parachute Inflation Research Experiments) project is investigating...
The Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project waslaunched to dev...
NASA's ASPIRE (Advanced Supersonic Parachute Inflation Research and Experiments) project is investig...
NASA's ASPIRE (Advanced Supersonic Parachute Inflation Research Experiments) project was launched to...
NASA's Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project was established...
The Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project waslaunched to dev...
The Advanced Supersonic Parachute Inflation Research and Experiment (ASPIRE) is a series of sounding...
Supersonic wind tunnel testing of Viking-type 0.8 m Disk-Gap-Band (DGB) parachutes was conducted in ...
Supersonic wind tunnel testing of 0.813 m diameter Disk-Gap-Band parachutes is being conducted in th...
Supersonic wind tunnel testing of Viking-type 0.8 m Disk-Gap-Band (DGB) parachutes was conducted in ...
A subsonic wind tunnel test was conducted to determine the drag and static aerodynamic coefficients,...
An overview of pre-flight aerodynamic models for the Low Density Supersonic Decelerator (LDSD) Super...
Inflation and drag characteristics of cross parachute in simulated Martian environmen
The Low Density Supersonic Decelerator Project is developing a next-generation supersonic parachute ...
Models are presented for the aerodynamic coefficients of Supersonic Ringsail and Disk-Gap-Band parac...
NASAs ASPIRE (Advanced Supersonic Parachute Inflation Research Experiments) project is investigating...
The Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project waslaunched to dev...
NASA's ASPIRE (Advanced Supersonic Parachute Inflation Research and Experiments) project is investig...
NASA's ASPIRE (Advanced Supersonic Parachute Inflation Research Experiments) project was launched to...
NASA's Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project was established...
The Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project waslaunched to dev...
The Advanced Supersonic Parachute Inflation Research and Experiment (ASPIRE) is a series of sounding...
Supersonic wind tunnel testing of Viking-type 0.8 m Disk-Gap-Band (DGB) parachutes was conducted in ...
Supersonic wind tunnel testing of 0.813 m diameter Disk-Gap-Band parachutes is being conducted in th...
Supersonic wind tunnel testing of Viking-type 0.8 m Disk-Gap-Band (DGB) parachutes was conducted in ...
A subsonic wind tunnel test was conducted to determine the drag and static aerodynamic coefficients,...
An overview of pre-flight aerodynamic models for the Low Density Supersonic Decelerator (LDSD) Super...
Inflation and drag characteristics of cross parachute in simulated Martian environmen
The Low Density Supersonic Decelerator Project is developing a next-generation supersonic parachute ...
Models are presented for the aerodynamic coefficients of Supersonic Ringsail and Disk-Gap-Band parac...