| 000 | 00718pam a2200193a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 005 | 20230109120555.0 | ||
| 008 | 230109b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aClark, Bruce J. | ||
| 245 | 1 | _aPROPELLANT VAPORIZATION AS A CRITERION FOR ROCKET-ENGINE DESIGN; EXPERIMENTAL PERFORMANCE, VAPORIZATION, AND HEAT-TRANSFER RATES WITH VARIOUS PROPELLANT COMBINATIONS [NASA MEMO 12-29-58E] | |
| 260 |
_bNational Aeronautics and Space Administration _c1959 _aWashington, D.C. |
||
| 300 | _a31p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound With Nasa Memo 12-8-58E-12-29-58E | ||
| 942 | _cTR | ||
| 999 |
_c398732 _d398732 |
||