Theoretical liquid propellant performance calculations
Archive copy is a photocopy.; The purpose of these writings is to compile in one volume the basic elements of thermodynamics and gas dynamics which are useful in the evaluation of thrust chamber performance. It is presumed that the reader will have had an elementary course in thermodynamics and gas...
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University of Alabama in Huntsville Archives
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| Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/10272 |
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Electronic |
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Saturn V Collection |
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University of Alabama in Huntsville Archives |
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University of Alabama in Huntsville Archives |
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Documents |
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Documents Theoretical liquid propellant performance calculations Misko, George |
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Documents Saturn project Saturn project Thermodynamics Liquid propellant rockets--Fuel tanks |
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Archive copy is a photocopy.; The purpose of these writings is to compile in one volume the basic elements of thermodynamics and gas dynamics which are useful in the evaluation of thrust chamber performance. It is presumed that the reader will have had an elementary course in thermodynamics and gas dynamics. The discussion of topics useful in evaluating thrust chamber performance is, of necessity, limited to these physical effects amenable to other areas that are as yet in the research stage of development. The author would like to take this opportunity to express his gratitude to Mr. G. S. Gill for many stimulating discussions on this subject. Thanks are due to Mr. D. J. Kuyper for permission to utilize his discussion on elastic-plastic strain and its application to nozzle throat area change. Finally, the author wishes to express his gratitude to his wife, Alice, who typed the bulk of the manuscript. |
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Theoretical liquid propellant performance calculationsMisko, GeorgeSaturn projectSaturn projectThermodynamicsLiquid propellant rockets--Fuel tanksArchive copy is a photocopy.; The purpose of these writings is to compile in one volume the basic elements of thermodynamics and gas dynamics which are useful in the evaluation of thrust chamber performance. It is presumed that the reader will have had an elementary course in thermodynamics and gas dynamics. The discussion of topics useful in evaluating thrust chamber performance is, of necessity, limited to these physical effects amenable to other areas that are as yet in the research stage of development. The author would like to take this opportunity to express his gratitude to Mr. G. S. Gill for many stimulating discussions on this subject. Thanks are due to Mr. D. J. Kuyper for permission to utilize his discussion on elastic-plastic strain and its application to nozzle throat area change. Finally, the author wishes to express his gratitude to his wife, Alice, who typed the bulk of the manuscript.1966-12-27TextPhysicsTheoliqupropperf.pdfspc_stnv_000901http://libarchstor2.uah.edu/digitalcollections/items/show/10272http://libarchstor2.uah.edu/digitalcollections/files/original/20/10272/Theoliqupropperf1.pdfSaturn V CollectionBox 20, Folder 42University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabamaenspc_stnv_000900_000924This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. |
| title |
Theoretical liquid propellant performance calculations |
| titleStr |
Theoretical liquid propellant performance calculations |
| author |
Misko, George |
| author_facet |
Misko, George |
| id |
UAHsaturnv10272 |
| url |
http://libarchstor2.uah.edu/digitalcollections/items/show/10272 |
| _version_ |
1790443372620546048 |