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Fracture Control Requirements for Composite and Bonded Vehicle and Payload Structures

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SUNS Notification Type
Correction
Organization that Developed the Standard
Organization that Developed the Standard
NASA Standard
Document Identifiers
Document Number
MSFC-RQMT-3479
Version
Baseline
Change Number
0
Document Date
Is Active?
ACTIVE
NASA Organization and Technical Discipline
Responsible NASA Organization
MSFC - Marshall Space Flight Center
Endorsed Standard
Endorsement Details
NASA Core Standard
No
NASA Endorsed Standard Status
Not NASA Endorsed
Mandatory Standard
NASA Mandatory Standard
Not a NASA Mandatory Standard
Document Scope
Document Scope
This document provides the fracture control requirements for composite and bonded structures
used in the construction of MSFC manned vehicle and payload hardware. The scope includes
manned launch, retrieval, transfer, and landing vehicles, space habitats, and payloads or
experiments that are launched, retrieved, stored, or operated during any portion of a manned
spaceflight mission.
Fiber reinforced polymer matrix composites, sandwich construction (bonded metallic and
nonmetallic), and bonds between metallic or composite parts fall within the scope of this
document.
Metal and ceramic matrix structures, foam, flexible inflatable structures, liquid-fueled rocket
engines, and solid propellants are specifically excluded. Also, fracture control of metallic
parts/structures are not specifically covered by this document, but where metallics are used in
conjunction with composites or bonds, all the provisions of this document shall be met.
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