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00979nam a2200193 a 4500 |
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767721 |
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20171111231140.0 |
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090129s1986 gr r 000 0 eng d |
040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
100 |
1 |
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|a Tauber, Michael, E.
|
245 |
1 |
0 |
|a Trajectory characteristics and heating of hypervelocity projectiles having large ballistic coeffients/
|c Michael E. Tauber
|
260 |
|
|
|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1986
|
300 |
|
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|a 17 σ. :
|b εικ. ;
|c 28 εκ.
|
490 |
0 |
|
|a NASA technical paper
|v 2614
|
650 |
|
0 |
|a Ballistic missiles
|x Atmospheric entry
|
710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Branch
|
710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch
|
710 |
2 |
|
|a Ames Research Center
|
952 |
|
|
|a GR-KoDPT
|b 59cc2aff6c5ad13446fa2b4a
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|