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080728s1974 gr r 000 0 eng d |
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|a GR-KoDPT
|b gre
|e AACR2
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100 |
1 |
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|a Martin, James A.
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|a A method for determining optimum phasing of a multiphase propulsion system for a single-stage vehicle with linearized inert weight/
|c by James A. Martin
|
260 |
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|a Washington:
|b NASA,
|c 1974
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300 |
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|a 24 σ. :
|b εικ. ;
|c 27 εκ.
|
490 |
0 |
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|a NASA technical note
|v 7792
|
504 |
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|a Βιβλιογραφία: σ. 17
|
650 |
|
0 |
|a Space vehicles
|x Propulsion systems
|x Mathematical models
|
650 |
|
0 |
|a Space shuttles
|
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 |
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|a Langley Research Center
|
952 |
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|a GR-KoDPT
|b 59cc2ecc6c5ad13446faa1d6
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|