TY  - RPRT
TI  - Hypersonic research engine project. Phase 2: Aerothermodynamic integration model, test plan, data item no. 2-2.01
AU  - Jilly, L. F.
PY  - 1972
UR  - https://ntrs.nasa.gov/citations/19740078519
ID  - 19740078519
ER  -