| 4.5.7-8-1 Ensure coupled loads analysis completed with a dynamic model of the Host Vehicle with Hosted Payload included |
Phase B |
Phase C |
Phase D1 |
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Ensure coupled loads analysis has been completed for all critical flight events using a dynamic model of the Host Vehicle with the Hosted Payload included. Structural dynamic interaction between the Hosted Payload and the Host Vehicle will alter the loads generated in coupled loads analysis for the Host Vehicle, Hosted Payload, and the launch vehicle.
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NA
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NA
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TOR-2014-02199, Guidelines for Hosted Payload Integration
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| 4.5.7-8-2 Ensure evaluation is completed for dynamic models used to calculate predicted loads for both the Host Vehicle and Hosted Payload |
Phase B |
Phase C |
Phase D1 |
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Ensure description of the dynamic properties of all payload structures including the Hosted Payload in terms of natural frequencies, associated mode shapes, and damping values. If the fundamental frequencies of the Hosted Payload are sufficiently high, it is possible that an accurate rigid body mass model could be used in place of a flexible dynamic model.
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NA
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NA
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TOR-2014-02199, Guidelines for Hosted Payload Integration
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