PRELUDE-EGSE
Electrical Ground Support Equipment
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Multi-function EGSE module PC104 Form factor
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Standalone operating or FlatSat-integrated
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Centralized power supply and data management for Flatsat
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Full platform physical interfaces (RBF, KS, OBF / Umbilical)
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Dedicated MCU for system control, monitoring, and automation
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Automated test execution and mission cycle simulation
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On-board SD card for data logging and post-processing
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Automated battery ground charging management
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Integrated battery bypass for direct PDU powering
PRELUDE-FLATSAT-1
Flatsat modular board
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Modular FlatSat platform for subsystem integration and testing
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PC104 Integration slots
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Up to 3 avionics system per module
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Current sensing monitoring for each module on I2C bus
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Electrical and data interconnections
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Supports EGSE module for centralized supply and control
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Optimized for system-level functional testing and AIT
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Reduces AIT time and integration complexity
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Expandable up to 5 boards (15x modules) with extension bridges
PRELUDE-TESTPOD
3U/6U/12U/16U Testpod
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Vibration qualification for CubeSat-class units
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Dynamic carriage for realistic lauch scenario simulation
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Adjustable preloads to replicate rail/clamp conditions
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High-fidelity launch-interface boundary conditions
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Supports qualification and acceptance test campaigns
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Compliant for NASA GEVS and ECSS test levels
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Repeatable, fast setup, and safe handling for AIT operations
