| 000 | 00615nam a22001697a 4500 | ||
|---|---|---|---|
| 005 | 20200212145716.0 | ||
| 008 | 200212b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aBuglia, Jmes J. and Newcomb, John F. | ||
| 245 |
_aA method for determinig the propellant required to maintain an earth orbital vehicle in a useful orbirt between two specified altitude limits [NASA TN D-1817] _cJames J. Buglia and John F. Newcomb |
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| 260 |
_aWashington, D. C. _bNASA _cAugust 1963 |
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| 300 | _a31p | ||
| 505 | _aTechnica note D-1817 | ||
| 700 | _aNewcomb, John F. | ||
| 942 | _cREF | ||
| 999 |
_c561338 _d561338 |
||