Assessment of Soil Modeling Capability for Orion Contingency Land Landing

• Published in: Journal of aerospace engineering Vol. 25; no. 1; pp. 125 - 131
• Main Authors: Heymsfield, Ernest, Fasanella, Edwin L, Hardy, Robin C, Boitnott, Richard L
• Format: Journal Article
• Language: English
• Published: American Society of Civil Engineers 01-01-2012
• Subjects: Computer simulation; Drop tests; Impact tests; Impact velocity; Landing; Mathematical models; Soil (material); Swing; TECHNICAL PAPERS
• ISSN: 0893-1321; 1943-5525
• DOI: 10.1061/(ASCE)AS.1943-5525.0000089

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
-15°
pitch, impacting a level soil mat at a
17.68  m/s
(58 fps) horizontal velocity and
1.52  m/s
(5 fps) vertical impact velocity. Three vertical drop tests were conducted with the boilerplate capsule at 0° pitch. Each test was conducted to measure the impact on a level soil mat with varying impact velocities:
3.66  m/s
,
7.31  m/s
, and
10.97  m/s
(12, 24, and 36 fps). Results of the study show the potential of using numerical modeling for vertical drop test and swing test simulations. Discrepancies between the numerical and experimental simulations primarily stem from the nonuniformity and complexity of soil behavior.