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20171111231047.0 |
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050519s1969 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 Childs, Gary A.
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| 245 |
1 |
0 |
|a Analysis of maximum range trajectories for rocket-propelled lunar flying vehicles in a uniform gravitational field/
|c by A. Gary Childs and Ernest S. Armstrong
|
| 260 |
|
|
|a Washington, D.C.:
|b National Aeronautics and Space Administration ,
|c 1969
|
| 300 |
|
|
|a 44 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
|
|a NASA technical note
|v NASA TN D-5475
|
| 500 |
|
|
|a "Langley Research Center"--σ.τ.
|
| 504 |
|
|
|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Space trajectories
|x Mathematical models
|
| 650 |
|
0 |
|a Space vehicles
|x Landing
|x Mathematical models
|
| 650 |
|
0 |
|a Space vehicles
|x Propulsion systems
|x Mathematical models
|
| 650 |
|
0 |
|a Lunar excursion module
|x Mathematical models
|
| 700 |
1 |
|
|a Armstrong, Ernest S.
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|
| 710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration
|
| 710 |
2 |
|
|a Langley Research Center
|
| 952 |
|
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|a GR-KoDPT
|b 59cc21896c5ad13446f8aab2
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
