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NASA KSC STD Z 0017 : 2014

Current
Current

The latest, up-to-date edition.

ENGINEERING ANALYSIS, THERMAL/FLUID, STANDARD FOR
Published date

01-01-2014

1. SCOPE
2. APPLICABLE DOCUMENTS
3. NOMENCLATURE AND DEFINITIONS
4. DOCUMENTATION AND SOFTWARE PACKAGES FOR THERMAL AND
   FLUID ANALYSIS
5. SOLUTION INDEPENDENCE AND SENSITIVITY
6. BOUNDING CONDITIONS AND DESIGN MARGINS
7. COMPONENT INPUTS
8. PIPING AND TUBING INPUTS
9. HEAT TRANSFER
APPENDIX A - REFERENCES FOR THERMOPHYSICAL PROPERTIES OF
             FLUIDS AND MATERIALS
APPENDIX B - SPECIFIC REFERENCES
APPENDIX C - THERMAL/FLUID DESIGN MARGINS
APPENDIX D - DERIVATION OF EQ. 15
APPENDIX E - KUTATELADZE EQUATION CORRECTION

Specifies the top-level requirements, methods, and boundary conditions that will be applied to all thermal and fluid analyses for systems designed and developed for use at John F. Kennedy Space Center (KSC), as well as for any spacecraft, instruments, and flight experiments designed and developed by KSC.

DocumentType
Standard
PublisherName
National Aeronautics and Space Administration
Status
Current

NASA KSC STD Z 0015 : 2014 ENGINEERING ANALYSIS, STANDARD FOR

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