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Fracture Control Requirements for Spaceflight Hardware

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Organization that Developed the Standard
Organization that Developed the Standard
NASA Standard
Document Identifiers
Document Number
NASA-STD-5019
Version
A w/CHANGE 4
Change Number
4
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
Endorsement Details
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
Fracture control shall be required on all human-rated space systems to preclude catastrophic failure. Fracture control provides a specialized methodology to address the consequences of naturally occurring and service-induced flaws, damage, or cracks in a part or structure. This document establishes the fracture control requirements for all human-rated spaceflight systems including payloads, propulsion systems, orbital support equipment, and planetary habitats.

This Standard establishes the fracture control requirements for human-rated spaceflight, since NASA policy states that fracture control be imposed on all human-rated spaceflight hardware. It was developed by a NASA-wide Fracture Control Working Group to provide a common framework for fracture control practices on NASA programs.
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