Rideshare payload user’s guide october 2022



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SpaceX Ride Share
6.6.9.3

COUPLED LOADS
SpaceX performs a CLA to verify the predicted dynamic flight loads and responses of the Payload are within the MPE described in Sections 3.3.2 and 3.3.3. If any results are found to exceed the MPE described in Sections 3.3.2 and 3.3.3,
SpaceX will provide the CLA results to the Customer for further evaluation.
6.6.9.4

PAYLOAD SEPARATION
SpaceX may perform a separation analysis for MicroSat-class Payload Constituents deploying from the Launch Vehicle to verify the Customer provided analysis as described in Section 2.3. CubeSat deployments from Containerized deployers are not specifically analyzed SpaceX instead relies on the separation properties provided by the Customer. These results are used as an input for the collision avoidance analysis. Since Payload mass properties and slosh are outside of SpaceX’s control, SpaceX will evaluate requirements compliance via the ideal analysis case. If required,
SpaceX will provide a presentation summarizing the results of the analysis and highlighting any issues or concerns for the Payload.
6.6.9.5

PAYLOAD CLEARANCE
SpaceX performs a clearance analysis to validate the dynamic envelope compatibility between the Launch Vehicle and the Payload, and the Co-Payload(s) to the Payload, during all phases of the Mission. Clearance analysis results will be provided to the Customer for any Payload in excess of the allowable Payload allowable volume defined in Appendix A.


RIDESHARE PAYLOAD USER’S GUIDE
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OPERATIONS
Launch Vehicle operations are described in this section for launches from CCSFS, KSC, and VSFB. SpaceX launch operations are designed for rapid response (targeting less than one hour from vehicle rollout from the hangar to launch. Customers are strongly encouraged to develop launch readiness capabilities and timelines consistent with a rapid prelaunch concept of operations.

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