| 000 | 00680nam a2200193 4500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 005 | 20220811123023.0 | ||
| 008 | 220811b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aNortham, G. Burton | ||
| 245 |
_aNASA TN [D-6923] _beffects of propellant composition variables on acceleration-induced burning-rate augmentation of solid propellants _cG. Burton Northam |
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| 260 |
_aWashington _bNational Aeronautics and Space Administration _c1972 |
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| 300 | _a32p | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aTechnical Note D-6920-6929 Bound Vol. No.101282; contents: TR9172-9180 | ||
| 650 | _aAerodynamics | ||
| 942 | _cTR | ||
| 999 |
_c565983 _d565983 |
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