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080623s1972 gr r 000 0 eng d |
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|a GR-KoDPT
|b gre
|e AACR2
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|a Henning, Allen B.
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|a Flight test of an erectable spacecraft used for decelerator testing at simulated Mars entry conditions/
|c by Allen B. Henning and Reginald R. Lundstrom
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| 260 |
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|a Washington:
|b National Aeronautics and Space Administration,
|c 1972
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| 300 |
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|a 57 σ. :
|b εικ. ;
|c 27 εκ.
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| 490 |
0 |
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|a NASA technical note
|v 6910
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| 504 |
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|a Βιβλιογραφία: σ. 22-24
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| 650 |
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0 |
|a Parachutes
|x Aerodynamics
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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 Lundstrom, Reginald R.
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| 710 |
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|a United States
|b National Aeronautics and Space Administration
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| 710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration
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| 710 |
2 |
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|a Langley Research Center
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| 952 |
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|a GR-KoDPT
|b 59cc2dbd6c5ad13446fa84e0
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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