RIDESHARE PAYLOAD USER’S GUIDE
© Space Exploration Technologies Corp. All rights reserved. No US. Export Controlled Data.
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SpaceX along with final report documentation.
In general, force-limited testing is allowed to a C
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value of five (5) or higher and must be in accordance with NASA-HDBK-7004C with a maximum notch depth of -10 dB. Notching is only permitted to prevent the Payload from exceeding the static load levels defined in Table 3-15. Notching to protect secondary structure or constituent responses is not permitted because that would result in an under-test as related to flight environments. A Mission-specific analysis will not be provided by SpaceX. Verification Testing is REQUIRED to the random vibration test levels and durations defined in Table 3-15 in accordance with the MPE defined in this section. This random vibration test can also be used to meet the design loads factors requirement defined in Section 3.3.2.
Table 3-7: Random Vibration MPE Frequency (Hz) Random Vibration MPE (P, All Axes
20 0.01 50 0.015 700 0.015 800 0.03 925 0.03 2000 0.00644
GRMS
5.57
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