US 11,987,394 B2
Multi-spacecraft deployment
Jon Brooks Upham, Longmont, CO (US)
Assigned to Maxar Space LLC, Palo Alto, CA (US)
Filed by Maxar Space LLC, Westminster, CO (US)
Filed on Sep. 23, 2022, as Appl. No. 17/952,050.
Prior Publication US 2024/0101281 A1, Mar. 28, 2024
Int. Cl. B64G 1/64 (2006.01)
CPC B64G 1/641 (2013.01) [B64G 1/643 (2023.08)] 20 Claims
OG exemplary drawing
 
1. A system comprising:
a plurality of spacecraft, wherein when in a stacked configuration the plurality of spacecraft are stacked above each other along a z-axis, wherein each spacecraft comprises one or more z-axis magnetic torque rods oriented along the z-axis, wherein collectively the one or more z-axis magnetic torque rods form a corresponding one or more sets of z-axis magnetic torque rods in which magnetic axes of the magnetic torque rods in each respective set are aligned with each other along the z-axis when the plurality of spacecraft are in the stacked configuration, wherein the one or more z-axis magnetic torque rods of a particular spacecraft is configured to interact with the Earth's magnetic field to provide torque to control orientation of the particular spacecraft; and
one or more circuits in communication with the z-axis magnetic torque rods of the plurality of spacecraft, wherein the one or more circuits are configured to:
operate each set of z-axis magnetic torque rods in a clamping configuration to maintain the plurality of spacecraft in the stacked configuration, wherein in the clamping configuration a north magnetic pole and a south magnetic pole of the z-axis magnetic torque rods in adjacent spacecraft in the stack face each other; and
operate the z-axis magnetic torque rods to deploy the plurality of spacecraft, including reverse a magnetic polarity of the one or more z-axis magnetic torque rods in a current top spacecraft in the stack to repel the current top spacecraft from the stack.