The Resource Characterization of real gas properties for space shuttle main engine fuel turbine and performance calculations, Gary J. Harloff ; [performing organization: Sverdrup Technology, Inc. ; sponsoring agency: National Aeronautics and Space Administration], (microform)

Characterization of real gas properties for space shuttle main engine fuel turbine and performance calculations, Gary J. Harloff ; [performing organization: Sverdrup Technology, Inc. ; sponsoring agency: National Aeronautics and Space Administration], (microform)

Label
Characterization of real gas properties for space shuttle main engine fuel turbine and performance calculations
Title
Characterization of real gas properties for space shuttle main engine fuel turbine and performance calculations
Statement of responsibility
Gary J. Harloff ; [performing organization: Sverdrup Technology, Inc. ; sponsoring agency: National Aeronautics and Space Administration]
Creator
Contributor
Subject
Language
eng
Summary
"Real thermodynamic and transport properties of hydrogen, steam, the SSME mixture, and air are developed. The SSME mixture properties are needed for the analysis of the space shuttle main engine fuel turbine. The mixture conditions for the gases, except air, are presented graphically over a temperature range from 800 to 1200° K, and a pressure range from 1 to 500 atm. Air properties are given over a temperature range of 320 to 500° K, which are within the bounds of the thermodynamics programs used, in order to provide mixture data which is more easily checked (than H2/H2O). The real gas property variation of the SSME mixture is quantified. Polynomial expressions, needed for future computer analysis, for viscosity, Prandtl number, and thermal conductivity are given for the H2/H2O SSME fuel turbine mixture at a pressure of 305 atm over a range of temperatures from 950 to 1140° K. These conditions are representative of the SSME turbine operation. Performance calculations are presented for the space shuttle main engine (SSME) fuel turbine. The calculations use the air equivalent concept. Progress towards obtaining the capability to evaluate the performance of the SSME fuel turbine, with the H2/H2O mixture, is described."--NTIS abstract
Member of
Cataloging source
COD
http://library.link/vocab/creatorDate
1945-
http://library.link/vocab/creatorName
Harloff, G. J.
Funding information
Prepared for Lewis Research Center under contract
Government publication
federal national government publication
Illustrations
illustrations
Index
no index present
Literary form
non fiction
Nature of contents
  • bibliography
  • technical reports
http://library.link/vocab/relatedWorkOrContributorName
  • Sverdrup Technology, Inc
  • United States
  • Lewis Research Center
Series statement
NASA contractor report
Series volume
175066
http://library.link/vocab/subjectName
  • Space shuttles
  • Rocket engines
  • Pump turbines
  • Gases, Real
  • Gas dynamics
  • Air
  • Fuel systems
  • Hydrogen fuels
  • Real gases
  • Rocket engines
  • Space Shuttle Main Engine
  • Steam
  • Thermodynamic properties
  • Transport properties
  • Turbine pumps
Label
Characterization of real gas properties for space shuttle main engine fuel turbine and performance calculations, Gary J. Harloff ; [performing organization: Sverdrup Technology, Inc. ; sponsoring agency: National Aeronautics and Space Administration], (microform)
Instantiates
Publication
Note
"June 1986."
Base of film
safety base undetermined
Bibliography note
Includes bibliographical references (pages 10-11)
Carrier category
microfiche
Carrier category code
he
Carrier MARC source
rdacarrier
Color
black and white
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Control code
ocm236225937
Dimensions
4x6 in. or 11x15 cm.
Emulsion on film
diazo
Extent
11 pages, 83 unnumbered pages
Form of item
microfiche
Generation
service copy
Media category
microform
Media MARC source
rdamedia
Media type code
h
Other physical details
illustrations.
Positive negative aspect
negative
http://bibfra.me/vocab/marc/reductionRatio
02
ReductionRatioRange
normal reduction
Reproduction note
Microfiche.
Specific material designation
microfiche
Stock number
N 86-27418
System control number
(Sirsi) a1133651
Label
Characterization of real gas properties for space shuttle main engine fuel turbine and performance calculations, Gary J. Harloff ; [performing organization: Sverdrup Technology, Inc. ; sponsoring agency: National Aeronautics and Space Administration], (microform)
Publication
Note
"June 1986."
Base of film
safety base undetermined
Bibliography note
Includes bibliographical references (pages 10-11)
Carrier category
microfiche
Carrier category code
he
Carrier MARC source
rdacarrier
Color
black and white
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Control code
ocm236225937
Dimensions
4x6 in. or 11x15 cm.
Emulsion on film
diazo
Extent
11 pages, 83 unnumbered pages
Form of item
microfiche
Generation
service copy
Media category
microform
Media MARC source
rdamedia
Media type code
h
Other physical details
illustrations.
Positive negative aspect
negative
http://bibfra.me/vocab/marc/reductionRatio
02
ReductionRatioRange
normal reduction
Reproduction note
Microfiche.
Specific material designation
microfiche
Stock number
N 86-27418
System control number
(Sirsi) a1133651

Library Locations

    • Central Library, Jesse H. Jones BuildingBorrow it
      500 McKinney St., Houston, TX, 77002, US
      29.759431 -95.369953
Processing Feedback ...