TY  - RPRT
TI  - A computer program to perform flow and thermal analysis during pressurization of the Space Shuttle Solid Rocket Motor field joint
AU  - Clayton, J. Louie
AU  - Colbert, R. F.
AU  - Ghaffarian, B.
AU  - Majumdar, Alok
PY  - 1991
UR  - https://ntrs.nasa.gov/citations/19910068953
ID  - 19910068953
ER  -