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LEADER |
01160nam a2200277 a 4500 |
001 |
725887 |
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20171111231102.0 |
008 |
050510m19769999gr r f000 0 eng d |
040 |
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|a GR-KoDPT
|b gre
|e AACR2
|
100 |
1 |
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|a Pirrello, C. J.
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245 |
1 |
0 |
|a Study of a fail-safe abort system for an actively cooled hypersonic aircraft/
|c C.J. Pirrello and R.L. Herring
|
260 |
|
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|a Washington, D.C.:
|b National Aeronautics and Space Administration,
|c 1976-
|
300 |
|
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|a τ. :
|b εικ. ;
|c 27 εκ.
|
490 |
0 |
|
|a NASA contractor report
|v NASA CR-2652
|
500 |
|
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|a "Prepared by McDonnell Aircraft Company for Langley Researh Center"
|
505 |
1 |
|
|a τ. 1. Technical summary
|
650 |
|
0 |
|a Hypersonic planes
|x Cooling
|x Equipment and supplies
|x Design and construction
|
650 |
|
0 |
|a Shielding (Heat)
|
650 |
|
0 |
|a Hydrogen as fuel
|
650 |
|
0 |
|a Airplanes
|x Speed
|
650 |
|
0 |
|a Aeronautics
|x Safety measures
|
700 |
1 |
|
|a Herring, R. L.
|
710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|
710 |
2 |
|
|a McDonnell Aircraft Company
|
710 |
0 |
|
|a Langley Research Center
|
952 |
|
|
|a GR-KoDPT
|b 59cc23556c5ad13446f8f973
|c 998a
|d 945l
|e TL 521 .3.C6 αρ.2652
|t 1
|x m
|z Books
|