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061009s1970 gr r l000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
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| 050 |
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|a QA299.3
|b .V3x
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| 082 |
|
0 |
|a 629.1/08 s
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| 100 |
1 |
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|a Velez, C. E.
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| 245 |
1 |
0 |
|a Derivation of Newtonian-type integration coefficients and some applications to orbit calculations/
|c by C.E. Velez and J.L. Maury ; Goddard Space Flight Center
|
| 260 |
|
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|a Washington:
|b National Aeronautics and Space Administration,
|c 1970
|
| 300 |
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|a iii, 50 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
|
|a NASA technical note
|v D-5958
|
| 650 |
|
0 |
|a Artificial satellites
|x Orbits
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| 700 |
1 |
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|a Maury, Jesse L.
|
| 710 |
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|a United States
|b National Aeronautics and Space Administration
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| 710 |
2 |
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|a Goddard Space Flight Center
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| 710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration
|
| 952 |
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|a GR-KoDPT
|b 59cc2d6d6c5ad13446fa7c47
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
