TY  - RPRT
TI  - Integrated Thermal Response Modeling System For Hypersonic Entry Vehicles
AU  - Chen, Y.-K.
AU  - Milos, F. S.
AU  - Partridge, Harry
PY  - 2000
UR  - https://ntrs.nasa.gov/citations/20010066108
ID  - 20010066108
ER  -