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060904s1970 gr r f000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
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| 100 |
1 |
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|a Miller, G. Kimball
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| 245 |
1 |
0 |
|a Fixed-base visual simulat5ion of obstacle avoidance during terminal descent of advanced Apollo spacecraft with an all-flexible parawing/
|c by G. Kimball Miller ; Langley Research Center
|
| 260 |
|
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|a Washington, D.C.:
|b National Aeronautics and Space Administration, Scientific and Technical Information Office,
|c 1970
|
| 300 |
|
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|a 49 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
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|a NASA technical note
|v D-5940
|
| 504 |
|
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|a Βιβλιογραφία: σ. 29
|
| 650 |
|
0 |
|a Airplanes
|x Parawings
|
| 650 |
|
0 |
|a Aerodynamics
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|
| 710 |
2 |
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|a Langley Research Center
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration
|
| 952 |
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|a GR-KoDPT
|b 59cc2c7d6c5ad13446fa647a
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
