RIDESHARE PAYLOAD USER’S GUIDE
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6 Payloads must target a minimum separation velocity of 0.3 ms and a maximum separation velocity of 1.0 ms. Containerized deployments such as CubeSats maybe deployed at a velocity greater than 1.0 ms. For Payloads that contain more than one deployment
, the separation velocities should be different between deployed Payload Constituents such that the fastest deployment is first. The Launch Vehicle is subject to the rotational rates in Table 2-1 prior to Payload separation. Table 2-1: Launch Vehicle Rates Before Payload Separation
Axis Rate Launch Vehicle Roll (W
± 2.0 deg/s Launch Vehicle Pitch (WY)
± 1.0 deg/s Launch Vehicle Yaw (W
± 1.0 deg/s 2.5Share with your friends: