Asic Specifications:

• • 150 kg smallsat
• • 330 km Sun Synchronous orbit
• • Electric propulsion
• • 300W pivoting solar panels
• • 6 year lifetime
• • Passive cold plate
• • Multi-core computer with ECC DRAM and FPGA
• • Two 2 TB NVMe solid state drives
• • 10 Gbps pixel bus
• • OLED selfie screen
• • Space selfie solar panel camera

Communications:

• • Globalstar radios for commands and telemetry
• • Optical uplink and downlink, multiple passes per day
• • Optical error corrected data transfers at 100 Mb/s
• • Custom optical ground stations
• • Small size, low weight, low power, and low complexity custom on-board satellite laser comm optics and electronics

Aiming/stabilization:

• • 4 momentum wheels
• • 4 control moment gyros
• • 3 magnetic torquers
• • 2 Star cameras
• • 2 GPS antennae, located on the opposite ends of the spacecraft

Optical Specifications:

• • Modified Dall-Kirkham telescope
• • 20" (50 cm) Zerodur primary mirror
• • 48 MP visible/NIR main camera with stellar guide chips and sub-pixel imager nanopositioners
• • 10 MP UV/visible/NIR high sensitivity camera with stellar guide chips and sub-pixel imager nanopositioners
• • 150 band hyper-spectral imager
• • 0.25 arc second IFOV
• • Native 40 cm GSD pan and multispectral
• • Super-resolution 30 cm GSD pan and multispectral

24 Position Filter Wheel:

• • Five stripe B, G, R, Red edge, I
• • Coastal Blue
• • polarizer
• • grism
• • H-alpha
• • H-beta
• • O-III
• • N-II
• • S-II
• • UV 200-300nm
• • Sloan u'
• • Sloan g'
• • Sloan r'
• • Sloan i'
• • Sloan z'