| 000 | 00691pam a2200217a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aChambellan, Rene E. | ||
| 245 | 1 | _aNASA Technical Note: COMPARATIVE STUDY OF FUSELAGE TANKS FOR LIQUID-METHANE-FUELED SUPERSONIC AIRCRAFT | |
| 260 |
_bNASA _c1968 _aWashington, D.C. |
||
| 300 | _a16p. | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note. | ||
| 500 | _aTechnical Note D-4831-4840 | ||
| 500 | _a Bound Vol. No.101114 contents TR7567-7575 | ||
| 650 | _aFlight-Weight Nonintegral Tanks | ||
| 653 | _aGage Pressures | ||
| 700 | _aBevevino, William A | ||
| 942 | _cTR | ||
| 999 |
_c393275 _d393275 |
||