The Micro-8 Platform
Space Inventor presents an advanced customizable microsatellite solution, crafted from modular Equipment for tailored missions. Our novel design reduces components, simplifying integration with easy 360° access.
The microsatellite platform is specifically engineered for the Falcon 9 quarter plate payload adapter and can utilize an 8-inch separation ring from ExoLaunch.
It is designed for reliability, and offers full flexibility to be adapted to specific customer needs. The platform features deployable solar panels with drive mechanism for optimal power generation further maximising the capabilities.
Your payload dimensions:
325 mm x 370 mm x 490 mm
Solar Array Configuration:
1 large rotating sun tracking solar panel per wing: 250 W
2 large rotating sun tracking solar panels per wing: 500 W
10 x Sun Sensors
Platform Mass:
35 kg
Redundant Radio Links:
2200 - 2290 MHz 10 Mbps downlink via S-band
7900 - 8400 MHz 100 Mbps downlink via X-band
Redundant Data Storage:
64 GB
Propulsion:
From 4.000 Ns - 30.000 Ns
Reaction Wheels:
4 x 1000 mNms / 100 mNm
Payload Data Interfaces:
CAN, Ethernet, RS422, SpaceWire, LVDS
Power:
Nominal voltage: 28 V
Capacity: 400 Whr
Dual hot redundant
Fully separated buses
Control Modes (using any
vector in body frame):
Nadir, Inertial, Sun Pointing,
Ground Spot Tracking, Ground Track
Dual mode (e.g. nadir + sun optimized tracking)
Attitude Determination:
2 x Star Trackers: Cross Bore Axis 1.5 arcsec
Bore axis 7 arcsec, 2 x Gyros, 2 x Magnetometers
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