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MSFC-STD-3744

STRUCTURAL DESIGN AND TEST STANDARD FOR SOLID ROCKET MOTORS

active, Most Current
Organization: MSFC
Publication Date: 21 January 2021
Status: active
Page Count: 24
scope:

This technical standard establishes baseline requirements for the structural design, and testing of SRMs. The requirements are limited to cases, solid propellants, insulators, liners, joint seals, ablatives and non-ablatives. These requirements may apply and be tailored to individual programs or projects with the agreement of the appropriate contractual and technical authorities in accordance with NPR 7120.5, NASA Space Flight Program and Project Management Requirements.

Applicability

This Standard is to be used to aid in the development of SRM design and test criteria. It meets the intent of higher-level NASA standards such as NASA-STD-5001.

This standard applies the following:

all mandatory actions (i.e., requirements) are denoted by statements containing the term, "shall", may" or "can" denote discretionary privilege or permission, "should" denotes a good practice and is recommended, but not required, "will" denotes expected outcome, and "are/is" denotes descriptive material.

Document History

MSFC-STD-3744
January 21, 2021
STRUCTURAL DESIGN AND TEST STANDARD FOR SOLID ROCKET MOTORS
This technical standard establishes baseline requirements for the structural design, and testing of SRMs. The requirements are limited to cases, solid propellants, insulators, liners, joint seals,...

References

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