Add to ORKGWind tunnel tests of inflatable disk-gap-band and modified ringsail parachutes at low dynamic pressur
Free-body tests were made in the Langley spin tunnel to determine drag coefficients for 1.07-meter-d...
A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...
Flight test of 30 foot nominal diameter cross parachute to measure shock loads, drag efficiency, and...
Ten flight tests of modified-ringsail, disk-gap-band, and cross parachute configurations with deploy...
Supersonic wind-tunnel tests were conducted with disk-gap-band parachute models having a nominal dia...
A subsonic wind tunnel test was conducted to determine the drag and static aerodynamic coefficients,...
Development and flight test of inflatable disk- gap-band parachute for high altitude deployment from...
Flight test of 40 foot parachute deployed at low supersonic speed and dynamic pressur
A 30-foot (9.1 meter) nominal-diameter disk-gap-band parachute (reference area 707 sq ft (65.7 m(exp...
Transonic wind-tunnel studies were conducted with modified cross, hemisflo, and disk-gap-band parach...
The Low Density Supersonic Decelerator project performed a wind tunnel experiment on the structural ...
Inflation, drag, and stability characteristics of 26-meter diameter ringsail parachute in simulated ...
A 31.2-foot (9.51 meter) nominal diameter (reference area 764 ft(exp 2) (71.0 m(exp 2)) ringsail par...
Flight test of disk-gap band parachute deployed at low supersonic speed and low dynamic pressure to ...
Models are presented for the aerodynamic coefficients of Supersonic Ringsail and Disk-Gap-Band parac...
Free-body tests were made in the Langley spin tunnel to determine drag coefficients for 1.07-meter-d...
A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...
Flight test of 30 foot nominal diameter cross parachute to measure shock loads, drag efficiency, and...
Ten flight tests of modified-ringsail, disk-gap-band, and cross parachute configurations with deploy...
Supersonic wind-tunnel tests were conducted with disk-gap-band parachute models having a nominal dia...
A subsonic wind tunnel test was conducted to determine the drag and static aerodynamic coefficients,...
Development and flight test of inflatable disk- gap-band parachute for high altitude deployment from...
Flight test of 40 foot parachute deployed at low supersonic speed and dynamic pressur
A 30-foot (9.1 meter) nominal-diameter disk-gap-band parachute (reference area 707 sq ft (65.7 m(exp...
Transonic wind-tunnel studies were conducted with modified cross, hemisflo, and disk-gap-band parach...
The Low Density Supersonic Decelerator project performed a wind tunnel experiment on the structural ...
Inflation, drag, and stability characteristics of 26-meter diameter ringsail parachute in simulated ...
A 31.2-foot (9.51 meter) nominal diameter (reference area 764 ft(exp 2) (71.0 m(exp 2)) ringsail par...
Flight test of disk-gap band parachute deployed at low supersonic speed and low dynamic pressure to ...
Models are presented for the aerodynamic coefficients of Supersonic Ringsail and Disk-Gap-Band parac...
Free-body tests were made in the Langley spin tunnel to determine drag coefficients for 1.07-meter-d...
A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...
Flight test of 30 foot nominal diameter cross parachute to measure shock loads, drag efficiency, and...