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Spacecraft Deployable Carbon-Composite Boom Thermal Distortion Lead *1#vT7n
Flatirons Orbital Structures @4&mR2k
Model thermal-vacuum bending distortion in deployable carbon-composite booms under solar radiation, calculate micro-yield strain limits in c... -
Spacecraft Launch Vehicle Thrust Vector Control Electronics Lead #8!kW5x
Mawson Defence Autonomy %3&qV7n
Design radiation-hardened servo amplifier circuits, redundant brushless motor driver electronics, and real-time ARINC 825 CAN bus interfaces...