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20151031170421.0 |
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041115s1983 cau bb f000 0 eng d |
| 035 |
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|a (OCoLC)ocm56968475
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| 037 |
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|a N 84-11318
|b NASA
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| 040 |
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|a GPO
|c GPO
|d MvI
|d UtOrBLW
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| 049 |
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|a UMIC
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| 074 |
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|a 0830-H-14 (MF)
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| 086 |
0 |
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|a NAS 1.26:171714
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| 100 |
1 |
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|a Schoenman, L.
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| 245 |
1 |
0 |
|a Combustion performance and heat transfer characterization of LOX/hydrocarbon type propellants :
|b final report, volume 2 /
|c prepared by L. Schoenman.
|
| 264 |
|
1 |
|a Sacramento, Calif. :
|b Aerojet Liquid Rocket Company,
|c [1983]
|
| 300 |
|
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|a 1 volume
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| 336 |
|
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|a text
|b txt
|2 rdacontent
|
| 337 |
|
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|a microform
|b h
|2 rdamedia
|
| 338 |
|
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|a microfiche
|b he
|2 rdacarrier
|
| 490 |
1 |
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|a NASA contractor report ;
|v NASA-CR-171714
|
| 500 |
|
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|a "Contract NAS 9-15958."
|
| 500 |
|
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|a "September 1983."
|
| 504 |
|
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|a Includes bibliographical references.
|
| 533 |
|
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|a Microfiche.
|b [Washington, D.C. :
|c National Aeronautics and Space Administration,]
|d 1984.
|e 3 microfiches.
|
| 500 |
|
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|a Microform.
|
| 650 |
|
7 |
|a Data bases.
|2 nasat
|
| 650 |
|
7 |
|a Heat transfer.
|2 nasat
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| 650 |
|
7 |
|a Injectors.
|2 nasat
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| 650 |
|
7 |
|a Liquid rocket propellants.
|2 nasat
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| 650 |
|
7 |
|a Oxygen-hydrocarbon rocket engines.
|2 nasat
|
| 650 |
|
7 |
|a Thermal stability.
|2 nasat
|
| 710 |
1 |
|
|a United States.
|b National Aeronautics and Space Administration.
|
| 830 |
|
0 |
|a NASA contractor report ;
|v NASA CR-171714.
|
| 999 |
|
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|a MARS
|
| 999 |
f |
f |
|s 9a50b14f-0362-39d9-aa2f-49badbd161e8
|i d8b34a37-6f00-3d3e-8b11-9c2500921e12
|t 0
|
| 952 |
f |
f |
|a Texas A&M University
|b College Station
|c Sterling C. Evans Library
|d Evans: US Documents Microfiche (3rd floor)
|t 0
|e NAS 1.26:171714
|h Superintendent of Documents classification
|
| 998 |
f |
f |
|a NAS 1.26:171714
|t 0
|l Evans: US Documents Microfiche (3rd floor)
|