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091210s1988 gr r 000 0 eng d |
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|a GR-KoDPT
|b gre
|e AACR2
|
100 |
1 |
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|a Masters, Philip A.
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245 |
1 |
0 |
|a High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion/
|c Philip A. Masters, Elizabeth S. Armstrong, and Harold G. Price
|
246 |
1 |
3 |
|a High pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion
|
260 |
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|a Washington:
|b National Aeronautics and Space Administration, Scientific and technical Information Division,
|c 1988
|
300 |
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|a 15 σ. :
|b εικ. ;
|c 27 εκ.
|
490 |
0 |
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|a NASA technical paper
|v 2862
|
650 |
|
0 |
|a Calorimeters
|
650 |
|
0 |
|a Combustion chambers
|
650 |
|
0 |
|a High pressure (Science)
|
650 |
|
0 |
|a Kerosene
|
650 |
|
0 |
|a Liquid oxygen
|
650 |
|
0 |
|a Oxygen-hydrocarbon rocket engines
|
650 |
|
0 |
|a RP-1 rocket propellants
|
700 |
1 |
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|a Armstrong, Elizabeth S.
|
700 |
1 |
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|a Price, Harold G.
|
710 |
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|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Division
|
710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Division
|
710 |
2 |
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|a Lewis Research Center
|
952 |
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|a GR-KoDPT
|b 59cc29df6c5ad13446f9f90c
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|