The Resource Rocket thrust chamber thermal barrier coatings : final report, by A.P. Batakis, J.W. Vogan for National Aeronautics & Space Administration, Communications & Propulsion Center, (microform)

Rocket thrust chamber thermal barrier coatings : final report, by A.P. Batakis, J.W. Vogan for National Aeronautics & Space Administration, Communications & Propulsion Center, (microform)

Label
Rocket thrust chamber thermal barrier coatings : final report
Title
Rocket thrust chamber thermal barrier coatings
Title remainder
final report
Statement of responsibility
by A.P. Batakis, J.W. Vogan for National Aeronautics & Space Administration, Communications & Propulsion Center
Creator
Contributor
Subject
Language
eng
Summary
"A research program was conducted to generate data and develop analytical techniques to predict the performance and reliability of ceramic thermal barrier coatings in high heat flux environments. A finite element model was used to analyze the thermomechanical behavior of coating systems in rocket thrust chambers. Candidate coating systems (using a copper substrate, NiCrAlY bond coat and ZrO2.8Y2O3 ceramic overcoat) were selected for detailed study based on photomicrographic evaluations of experimental test specimens. ... Thermal conductivity, strain tolerance, density, and residual stress were measured for these coatings. Analyses indicated that extremely thin coatings ( 0.02 mm) are required to accommodate the high heat flux of a rocket thrust chamber and ensure structural integrity."--NTIS abstract
Member of
Cataloging source
COD
http://library.link/vocab/creatorName
Batakis, Anthony P
Funding information
Prepared for National Aeronautics and Space Administration, Communications & Propulsion 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
Period covered
Dec. 1981 - Oct. 1984.
http://library.link/vocab/relatedWorkOrContributorName
  • Vogan, J. W
  • Solar Turbines International
  • Caterpillar Tractor Company
  • United States
Series statement
NASA CR
Series volume
175022
http://library.link/vocab/subjectName
  • Ceramic coating
  • Rockets (Aeronautics)
  • Rocket engines
  • Ceramics
  • Finite element method
  • Prediction analysis techniques
  • Thermal control coatings
  • Thrust chambers
Type of report
Final report;
Label
Rocket thrust chamber thermal barrier coatings : final report, by A.P. Batakis, J.W. Vogan for National Aeronautics & Space Administration, Communications & Propulsion Center, (microform)
Instantiates
Publication
Note
"July 1985."
Base of film
safety base undetermined
Bibliography note
Includes bibliographical references (pages 111-112)
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
ocm231642074
Dimensions
4x6 in. or 11x15 cm.
Emulsion on film
diazo
Extent
xii, 164 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 86-20497
System control number
(Sirsi) a1133645
Label
Rocket thrust chamber thermal barrier coatings : final report, by A.P. Batakis, J.W. Vogan for National Aeronautics & Space Administration, Communications & Propulsion Center, (microform)
Publication
Note
"July 1985."
Base of film
safety base undetermined
Bibliography note
Includes bibliographical references (pages 111-112)
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
ocm231642074
Dimensions
4x6 in. or 11x15 cm.
Emulsion on film
diazo
Extent
xii, 164 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 86-20497
System control number
(Sirsi) a1133645

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