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Fracture Control Requirements for Payloads Using the Space Shuttle

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NASA Standard
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NASA-STD-5003
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Baseline
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OCE - Office of the Chief Engineer
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5000 - Structures/Mechanical Systems, Fluid Dynamics, Thermal, Propulsion, Aerodynamics
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Not NASA Endorsed
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Document Scope
The purpose of this document is to establish the fracture control requirements for all payload hardware to be launched or retrieved using the Space Shuttle. Meeting these requirements implements the minimum fracture control requirements of National Space Transportation System (NSTS) 1700.7, Safety Policy and Requirements for Payloads Using the Space Transportation System. All payload fracture control shall be in accordance with the requirements stated herein.
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Fracture Control Requirements for Payloads Using the Space Shuttle
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NASA-STD-5003-10-7-96-Cancelled.pdf (451.99 KB)
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Last modified by:  Brenda K Bailey
Last modified on:  Mon, 12/19/2022 - 11:33

 

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