RIDESHARE PAYLOAD USER’S GUIDE
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2 PERFORMANCE 2.1 MASS PROPERTIES Payloads must comply with the mass and X
PL
center of gravity limitations given in Figure 2-1. Y
PL
and Z
PL
center of gravity dimensions must fall within the mechanical interface diameter for the Payload. The Payload coordinate frame is defined in Section 4.2.3.
Figure 2-1: Allowable Payload Mass and XPL Center of Gravity The Launch Vehicle maybe able to accommodate payloads with characteristics outside the limitations
indicated in this section, on a case by case basis. Mass property capabilities maybe further constrained by mission- unique Payload adapters,
dispensers, or separation systems.
2.2 LAUNCH WINDOWS The Launch Vehicle is capable of
launching any day of the year, at anytime of day, subject to environmental limitations and constraints as well as range availability and readiness within the SpaceX-determined Launch Period. Launch Window times and durations are developed specifically for each Mission. Customers may benefit from recycle operations (reference Section 7.5.5), maximizing launch opportunities within the Launch Window.
RIDESHARE PAYLOAD USER’S GUIDE
© Space Exploration Technologies Corp. All rights reserved. No US. Export Controlled Data.
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