A spacecraft, comprising: a centrally-oriented core, comprising: a computing device, comprising: a processor; and a memory, coupled to the processor, comprising computer instructions to control the spacecraft; a power source, coupled to the core; a plurality of struts, each comprising a root end coupled to the core and a distal end, the plurality of struts extending radially from the core; a plurality of blade deployers, coupled to distal ends of the plurality of struts, each comprising: a blade roll, oriented between a pair of end caps and configured to store a blade in a rolled disposition prior to blade deployment and unroll the blade to an extended disposition to deploy the blade, a blade deployment actuator, disposed between an end cap and the blade roll, configured to be controlled by the computing device and configured to rotate the blade roll to deploy or store the blade, a blade assembly yoke, coupled to the end caps to provide structural support to the blade deployer, a pitch actuator, configured to be controlled by the computing device and configured to pitch a corresponding blade a number of degrees, and a blade clamp, configured to clamp or unclamp the blade to the blade roll, comprising: a blade clamp actuator, configured to be controlled by the computing device and configured to unclamp an undeployed portion of the blade from the blade roll to deploy the blade and clamp the blade to the blade roll to pitch or store the blade; and a plurality of blades, coupled to the plurality of blade deployers and extending radially away from the core and in a common plane with the plurality of struts, the plurality of blades comprising material configured to be deflected by solar pressure, each of the struts configured to provide damping to a corresponding blade. a computing device, comprising: a processor; and a memory, coupled to the processor, comprising computer instructions to control the spacecraft; a processor; and a memory, coupled to the processor, comprising computer instructions to control the spacecraft; a power source, coupled to the core; a plurality of struts, each comprising a root end coupled to the core and a distal end, the plurality of struts extending radially from the core; a plurality of blade deployers, coupled to distal ends of the plurality of struts, each comprising: a blade roll, oriented between a pair of end caps and configured to store a blade in a rolled disposition prior to blade deployment and unroll the blade to an extended disposition to deploy the blade, a blade deployment actuator, disposed between an end cap and the blade roll, configured to be controlled by the computing device and configured to rotate the blade roll to deploy or store the blade, a blade assembly yoke, coupled to the end caps to provide structural support to the blade deployer, a pitch actuator, configured to be controlled by the computing device and configured to pitch a corresponding blade a number of degrees, and a blade clamp, configured to clamp or unclamp the blade to the blade roll, comprising: a blade clamp actuator, configured to be controlled by the computing device and configured to unclamp an undeployed portion of the blade from the blade roll to deploy the blade and clamp the blade to the blade roll to pitch or store the blade; and a plurality of blades, coupled to the plurality of blade deployers and extending radially away from the core and in a common plane with the plurality of struts, the plurality of blades comprising material configured to be deflected by solar pressure, each of the struts configured to provide damping to a corresponding blade. a blade roll, oriented between a pair of end caps and configured to store a blade in a rolled disposition prior to blade deployment and unroll the blade to an extended disposition to deploy the blade, a blade deployment actuator, disposed between an end cap and the blade roll, configured to be controlled by the computing device and configured to rotate the blade roll to deploy or store the blade, a blade assembly yoke, coupled to the end caps to provide structural support to the blade deployer, a pitch actuator, configured to be controlled by the computing device and configured to pitch a corresponding blade a number of degrees, and a blade clamp, configured to clamp or unclamp the blade to the blade roll, comprising: a blade clamp actuator, configured to be controlled by the computing device and configured to unclamp an undeployed portion of the blade from the blade roll to deploy the blade and clamp the blade to the blade roll to pitch or store the blade; and a plurality of blades, coupled to the plurality of blade deployers and extending radially away from the core and in a common plane with the plurality of struts, the plurality of blades comprising material configured to be deflected by solar pressure, each of the struts configured to provide damping to a corresponding blade. a blade clamp actuator, configured to be controlled by the computing device and configured to unclamp an undeployed portion of the blade from the blade roll to deploy the blade and clamp the blade to the blade roll to pitch or store the blade; and a plurality of blades, coupled to the plurality of blade deployers and extending radially away from the core and in a common plane with the plurality of struts, the plurality of blades comprising material configured to be deflected by solar pressure, each of the struts configured to provide damping to a corresponding blade.