| 000 | 00559 a2200157 4500 | ||
|---|---|---|---|
| 005 | 20221228110124.0 | ||
| 100 | _aSmith, G. Louis | ||
| 245 |
_aVortex flow and erosion on rocket nozzles due to warm-gas injection for thrust vector control[NASA TN D-3242] _cG. Louis Smith |
||
| 260 |
_aWashington,D.C. _bNatoonal Aeronautics and Space Adminstartion _c1966 |
||
| 300 | _a23p | ||
| 440 | _aNational Aeronautics and Space Adminstration | ||
| 440 | _aNASA technical note | ||
| 500 | _aBound vol. contains D 3241-3250 | ||
| 650 | _aRocket nozzles | ||
| 942 | _cTR | ||
| 999 |
_c566365 _d566365 |
||