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NASA STD-I-5019

Fracture Control Requirements for Spaceflight Hardware

standard by National Aeronautics and Space Administration , 09/22/2006

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Full Description

Fracture control is implemented to reduce the risk of a catastrophic failure from a defect or damage. The intent of this standard is to provide fracture control requirements for spaceflight hardware. A variety of fracture control considerations and options are addressed, some of which may not be applicable to a given design. Information is provided to assist the user in the development of an effective Fracture Control Plan and other fracture control documentation.
 

Product Details

Edition:
Baseline
Published:
09/22/2006
Number of Pages:
40
File Size:
1 file , 140 KB
 

Document History

  1. NASA STD-5019 Rev. A w/Change 1


    Fracture Control Requirements for Spaceflight Hardware, w/Change 1: Administrative Change 2016-02-26

    • Historical Version

  2. NASA STD-5019 Rev. A w/Change 3


    Fracture Control Requirements for Spaceflight Hardware w/Change 3, Revalidation with Editorial/Administrative Changes (2020-08-14)

    • Most Recent

  3. NASA STD-5019 Rev. A w/Change 2


    Fracture Control Requirements for Spaceflight Hardware, w/ Change 2: Administrative Change 2018-03-29

    • Historical Version

  4. NASA STD-5019 Rev. A


    Fracture Control Requirements for Spaceflight Hardware

    • Historical Version

  5. NASA STD-5019


    Fracture Control Requirements for Spaceflight Hardware

    • Historical Version

  6. NASA STD-I-5019

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    Fracture Control Requirements for Spaceflight Hardware

    • Historical Version