Validation for Spaceflight Testing
Wright-Patterson Air Force Base · Space · Client: Wright-Patterson Air Force Base / USAF Armstrong
Project details
Conducted finite element validation simulations using horizontal impulse accelerator and vertical deceleration tower test matrices. Simulations evaluated the GHBMC 50th male simplified occupant (M50-OS), Hybrid III, and THOR 50th male FE models in LS-DYNA to predict injury risks in spaceflight-like loading conditions.
