Rideshare payload user’s guide october 2022
PAYLOAD MANEUVERS AND DEPLOYMENTS
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| PAYLOAD MANEUVERS AND DEPLOYMENTS Payloads must adhere to the following keep outs Delay attitude maneuvers until at least 120 seconds after Payload separation from the Launch Vehicle Delay mechanical appendage deployment (e.g. solar panel deployment) until at least 120 seconds after Payload separation from the Launch Vehicle o For any mechanical appendage deployment within first 24 hours, Customer must communicate to SpaceX abounding hard body radius for the Payload. Delay secondary deployments (e.g. a deployed object deploying a sub-Payload) until at least seven days after Payload separation from the Launch Vehicle Delay propulsive maneuvers until at least seven days after Payload separation All secondary deployments must be performed while under active attitude control. Deployments in uncontrolled directions are not allowed. The seven-day period allows adequate time for external cataloging of all Co-Payloads deployed from the Launch Vehicle and sufficient orbital spreading before additional release of Payload Constituents or orbital maneuvers. It is the Customers responsibility to pre-coordinate orbital maneuvers or the secondary deployment of Payload Constituents with the 18th Space Control Squadron (SPCS), submit estimated trajectories for screening to the 18th SPCS, and demonstrate to SpaceX that coordination with the 18th SPCS has been completed. See Section 6.5.7 for information on Coordination with Space Situational Awareness Agencies. RIDESHARE PAYLOAD USER’S GUIDE © Space Exploration Technologies Corp. All rights reserved. No US. Export Controlled Data. 7 3 ENVIRONMENTS The Launch Vehicle has been designed to provide a benign Payload environment. The environments presented below reflect typical Mission maximum predicted environments (MPE) for Payloads. Mission-specific analyses will be performed by SpaceX as indicated in Section 6.6.9. 3.1 TRANSPORTATION ENVIRONMENTS Transportation environments at launch facilities will be enveloped by the flight environments in Section 3.3. Download 2.78 Mb. Share with your friends:
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