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Strength Design and Verification Criteria for Glass, Ceramics, and Windows in Human Space Flight Applications

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Organization that Developed the Standard
Organization that Developed the Standard
NASA Standard
Document Identifiers
Document Number
NASA-STD-5018
Version
Baseline w/CHANGE 1
Change Number
1
Document Date
Change Date
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ACTIVE
NASA Organization and Technical Discipline
Responsible NASA Organization
NASA HQ, Office, Facility or Division
NASA HQ Office, Facility or Division
OCE - Office of the Chief Engineer
Technical Discipline Category
5000 - Structures/Mechanical Systems, Fluid Dynamics, Thermal, Propulsion, Aerodynamics
Endorsed Standard
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Endorsing NASA Organization
OCE Endorsed Standard
NASA Core Standard
No
NASA Endorsement Date
NASA Endorsed Standard Status
NASA Endorsed Standard
Mandatory Standard
NASA Mandatory Standard
Not a NASA Mandatory Standard
Document Scope
Document Scope
The purpose of this Standard is to specify the minimum structural design requirements for the design, development, and verification of windows, glass, and ceramic structure included in National Aeronautics and Space Administration (NASA) vehicles/elements, habitats, space suits, all orbital support equipment (OSE), and flight support equipment (FSE). Although this Standard primarily addresses structural design requirements for glass and ceramics, it also includes design and verification requirements for non-structural glass and ceramic components. Optical performance and radiation specifications are not provided in this document.
Keywords
Strength Design and Verification Criteria for Glass, Ceramics, and Windows in Human Space Flight Applications.
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Next 5-Year Review Date
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System Admin
Submitting User's Email
standards@msfc.nasa.gov

Last modified by:  Fred McMullen
Last modified on:  Sun, 10/15/2023 - 01:10

 


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