TY  - RPRT
TI  - Modeling Uprighting of the Orion Crew Module using a Finite Element Method with Wave Coupling and Structural Deformability
AU  - John Puryear
AU  - Shreyas Joglekar
AU  - Tannen VanZwieten
AU  - Troy Lyons
UR  - https://ntrs.nasa.gov/citations/20230017064
ID  - 20230017064
ER  -