Nasa expendable launch vehicle payload safety requirements: requirements table


HANDLING STRUCTURES INITIAL AND PERIODIC TEST REQUIREMENT FLOW PATH



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HANDLING STRUCTURES INITIAL AND PERIODIC TEST REQUIREMENT FLOW PATH


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Figure A2.1 Flow Path

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Figure A2.1 Flow Path (page 2)

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NOTES:

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1. Design, Fabrication, and In-Process Requirements:

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a. Meet NASA-STD-8719.9 and AFSPCMAN 91-710 design requirements for handling structures.

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b. Identify SFP components and SFP welds.

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2. Perform 100 percent visual inspection of all components (including SFP) and weld joints (including SFP and non-SFP) and perform 100 percent surface NDE testing of all SFP components and SFP welds.

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3. Perform volumetric NDE on 4 inches or 10 percent (whichever is less) of every continuous, non-SFP, full penetration weld in accordance with AWS D14.1 paragraph 10.9.5 or paragraph 10.13.6.

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4. Cycle count is required.

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5. MHE and MHSE that has been in service for 10 years or 2,500 cycles, whichever is less, shall be evaluated against current standards and requirements.

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6. Perform safe-live analysis assuming flaws to be in the worst location (transition areas, heat affected areas, weld joints, membrane sections, and highest stressed areas). Safe-life analysis shall be performed using fatigue crack growth computer programs such as NASA/FLAGRO (JSC-22267) or other PSWG and Range Safety Approved computer programs or analysis methods.

Note: Fracture mechanics analysis used to establish cyclic limits may assume "crack-like defects." This assumption does not imply that cracks or other rejectable indications are acceptable. The logic identified in this flow chart requires that cracks and rejectable indications be fixed.



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7. Provide noncompliance issues, if any, to PSWG for PSWG and Range Safety disposition.

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8. All parts shall be considered to have low-fracture toughness with a material property ratio Kic/Fty<0.33 in 1/2. If the part is a steel bolt and the Kic value is unknown, low fracture toughness shall be assumed when Ftu > 180 ksi. Where: Kic = Plane strain fracture toughness Fty = Allowable tensile yield strength Ftu = Allowable tensile ultimate strength

Reference: NASA NBH 8071.1











9. Fix hardware. This means either repair or an analytical solution is required as approved by the PSWG and Range Safety.

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10. Periodic test and inspection requirements are identified in the gray areas of the flow chart. All the processes identified in the figure are considered initial test requirements.

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11. Proof test shall be performed on fully assembled handling structures, unless otherwise approved by the PSWG and Range Safety. Do not proof test greater than 85 percent of yield.

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12. Perform NDE in accordance with the PSWG and Range Safety approved NDE plan.

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