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01154nam a2200229 a 4500 |
| 001 |
767940 |
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20171111231140.0 |
| 008 |
090127s1987 gr r 000 0 eng d |
| 040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
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|a Smith, Tamara A.
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| 245 |
1 |
0 |
|a Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m2(350 psia)/
|c Tamara A. Smith, Albert J. Pavli, and Kenneth J. Kacynski
|
| 260 |
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Office,
|c 1987
|
| 300 |
|
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|a 21 σ. :
|b εικ. ;
|c 28 εκ.
|
| 490 |
0 |
|
|a NASA technical paper
|v 2725
|
| 650 |
|
0 |
|a Rocket engines
|
| 650 |
|
0 |
|a Rockets (Aeronautics)
|x Nozzles
|
| 700 |
1 |
|
|a Pavli, Albert J.
|
| 700 |
1 |
|
|a Kacynski, Kenneth J.
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Office
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Office
|
| 710 |
2 |
|
|a Lewis Research Center
|
| 952 |
|
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|a GR-KoDPT
|b 59cc2b056c5ad13446fa2c33
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
