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20171111231046.0 |
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050715s1987 gr r f000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
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|a Hartman, Edward R.
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| 245 |
1 |
0 |
|a Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65/
|c Edward R. Hartman, Patrick J. Johnston
|
| 246 |
1 |
3 |
|a Mach six experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰
|
| 260 |
|
|
|a [Washington, D.C.]:
|b National Aeronautics and Space Administration, Scientific and Technical Information Office,
|c 1987
|
| 300 |
|
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|a 38 σ. :
|b εικ. ;
|c 28 εκ.
|
| 490 |
0 |
|
|a NASA technical paper
|v 2733
|
| 504 |
|
|
|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Guided missiles
|x Stability
|
| 700 |
1 |
|
|a Johnston, Patrick J.
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Office
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|
| 710 |
0 |
|
|b Scientific and Technical Information Office
|
| 952 |
|
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|a GR-KoDPT
|b 59cc21426c5ad13446f8a188
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
