| contributor author | Ernest Heymsfield | |
| contributor author | Edwin L. Fasanella | |
| contributor author | Robin C. Hardy | |
| contributor author | Richard L. Boitnott | |
| date accessioned | 2017-05-08T21:33:47Z | |
| date available | 2017-05-08T21:33:47Z | |
| date copyright | January 2012 | |
| date issued | 2012 | |
| identifier other | %28asce%29as%2E1943-5525%2E0000089.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56232 | |
| description abstract | Twenty-one swing tests were conducted at the NASA Langley Landing and Impact Research (LandIR) Facility in 2006 to evaluate Orion boilerplate ground landings as a function of impact velocity and pitch. In this article, experimental results from two capsule swing tests and three vertical drop tests are compared with numerical results. The numerical results were derived by using the nonlinear dynamic finite-element code LS-DYNA. The swing tests were conducted at 0° and | |
| publisher | American Society of Civil Engineers | |
| title | Assessment of Soil Modeling Capability for Orion Contingency Land Landing | |
| type | Journal Paper | |
| journal volume | 25 | |
| journal issue | 1 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000089 | |
| tree | Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 001 | |
| contenttype | Fulltext | |
