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970102s1966 dcu 000 0 eng d |
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|a (MdBJ)1985524
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|a (OCoLC)36150429
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|a (OCoLC-I)681727710
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|a BNA:11/25/97
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|a GZM
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|a GZM
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|a JHEE
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4 |
|a TL521
|b .A3312 no.236
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|a NAS 1.12:236
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086 |
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|a NAS 1.12:236
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100 |
1 |
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|a Seiff, Alvin
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245 |
1 |
0 |
|a Minimization of the total heat input for manned vehicles entering the earth's atmosphere at hyperbolic speeds /
|c by Alvin Seiff and Michael E. Tauber
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260 |
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|a Washington, D.C. :
|b National Aeronautics and Space Administration,
|c 1966
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300 |
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|a i, 56 p. :
|b ill. ;
|c 27 cm
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490 |
1 |
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|a NASA technical report ;
|v NASA TR R-236
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590 |
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|a Copy 1 bound with v. R-223
|c 8723902 (parent records ckey)
|b 36105024742178 (item id)
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|a 31
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|a Conical shells
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|a Heat
|x Radiation and absorption
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650 |
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0 |
|a Space vehicles
|x Atmospheric entry
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700 |
1 |
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|a Tauber, Michael E
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830 |
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0 |
|a NASA technical report ;
|v R-236
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