Add to ORKGSpacecraft are being designed based on LS-DYNA simulations of water landing impacts. The Elemental Water Impact Test (EWIT) series was undertaken to assess the accuracy of LS-DYNA water impact simulations. Phase 1 of the EWIT series featured water impact tests of a 20-inch hemisphere dropped from heights of 5 feet and 10 feet. The hemisphere was outfitted with an accelerometer and three pressure gages. The focus of this report is the correlation of analytical models against test data
A series of crash tests were conducted with dummies during simulated Orion crew module landings at t...
The NASA Emergency Locator Transmitter Survivability and Reliability (ELTSAR) project was initiated ...
Water droplet impingement data were obtained at the NASA Glenn Icing Research Tunnel (IRT) for a 36-...
Spacecraft are being designed based on LS-DYNA simulations of water landing impacts. The Elemental W...
Spacecraft are being designed based on LS-DYNA water landing simulations. The Elemental Water Impact...
The Ground Test Article (GTA) is an early production version of the Orion Crew Module (CM). The stru...
Crew Exploration Vehicle (CEV) water splashdowns were simulated in order to find maximum acceleratio...
During 2003 and 2004, the Johnson Space Center's White Sands Testing Facility in Las Cruces, New Mex...
During the space shuttle return-to-flight preparations following the Columbia accident, finite eleme...
A total of 59 tail first drops were made. Model entry conditions simulated full scale vertical veloc...
Automatic water monitor system was tested with the objectives of assuring high-quality effluent stan...
During the summer of 2015, three Cessna 172 aircraft were crash tested at the Landing and Impact Res...
Preliminary results from the heavily instrumented ALF502R-5 engine test conducted in the NASA Glenn ...
A study of the Weber Number effects on droplets in the NASA Icing Research Tunnel is described. The ...
The design and certification of modern transport airplanes for flight in icing conditions increasing...
A series of crash tests were conducted with dummies during simulated Orion crew module landings at t...
The NASA Emergency Locator Transmitter Survivability and Reliability (ELTSAR) project was initiated ...
Water droplet impingement data were obtained at the NASA Glenn Icing Research Tunnel (IRT) for a 36-...
Spacecraft are being designed based on LS-DYNA simulations of water landing impacts. The Elemental W...
Spacecraft are being designed based on LS-DYNA water landing simulations. The Elemental Water Impact...
The Ground Test Article (GTA) is an early production version of the Orion Crew Module (CM). The stru...
Crew Exploration Vehicle (CEV) water splashdowns were simulated in order to find maximum acceleratio...
During 2003 and 2004, the Johnson Space Center's White Sands Testing Facility in Las Cruces, New Mex...
During the space shuttle return-to-flight preparations following the Columbia accident, finite eleme...
A total of 59 tail first drops were made. Model entry conditions simulated full scale vertical veloc...
Automatic water monitor system was tested with the objectives of assuring high-quality effluent stan...
During the summer of 2015, three Cessna 172 aircraft were crash tested at the Landing and Impact Res...
Preliminary results from the heavily instrumented ALF502R-5 engine test conducted in the NASA Glenn ...
A study of the Weber Number effects on droplets in the NASA Icing Research Tunnel is described. The ...
The design and certification of modern transport airplanes for flight in icing conditions increasing...
A series of crash tests were conducted with dummies during simulated Orion crew module landings at t...
The NASA Emergency Locator Transmitter Survivability and Reliability (ELTSAR) project was initiated ...
Water droplet impingement data were obtained at the NASA Glenn Icing Research Tunnel (IRT) for a 36-...