UGA GA’s Leap to Sp Space: Sm Small Satel ellite e Res esea earch Lab Te Testing By Niklas Endler
Th The Te Team
Small ll Satelli llites
SPOC C and M MOCI CI ^(Multiview Onboard Computational Imager)
Low E Eart rth Orb rbit - LEO EO
Env nvironm nment ntal F Factors - vacuum - radiation - intense and r rapid temperature r change - etc
UNP UNP - Testing ng S Standa ndards ds
The C e Chamber er 10 inch flange for mounting shroud Pressure Gauge Turbo Pump
The Ch Chamber CA CAD - Fu Full 10 inch flange for mounting shroud
The Ch Chamber CA CAD - Se Section
Old C d Conc ncept Designs ns
Fina nal S Shr hroud d Design 10 inch flange for mounting shroud
Final R l Result lt Funnel Heating Elements 3D Printed Satellite
Ther ermocouples es ^looking through the 10 Arduino inch flange - 6 wires
Nex ext S Step eps - Pressure tight vacuum chamber - Mounted thermocouples - Run and test thermal shroud performance in nitrogen and vacuum environments - ^ with satellite
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