TY  - RPRT
TI  - Finite Element Simulation of a Space Shuttle Solid Rocket Booster Aft Skirt Splashdown Using an Arbitrary Lagrangian-eulerian Approach
AU  - Melis, Matthew E.
PY  - 2003
UR  - https://ntrs.nasa.gov/citations/20030016601
ID  - 20030016601
ER  -