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Flight-grade onboard compute built on high-reliability FPGAs with RISC-V cores. One standardised compute platform serves the on-board computer, engine controller, and high-rate test-site roles, scaling from bench to flight without redesign.

A complete sensor instrumentation set for launch-vehicle test and flight: temperature, current loop, fast-sampled signals, bridge, accelerometer, and binary I/O channels in a single modular form factor. Every input carries miswiring detection and over- and under-voltage protection as standard.

Communication fabric for the launch-vehicle avionics stack, spanning RS422/485, deterministic Ethernet (IEEE 1588 PTP and TSN), CAN-FD and CAN-XL, SpaceWire, fibre, and wireless. Mixed-protocol topologies are addressed by one modular bus interface family rather than a stack of vendor-specific cards.

Mission-specific functions outside the general compute, instrumentation, and networking pattern: S-band telemetry downlink, GNSS positioning and timing, multi-hundred-gigabyte onboard storage, and H.264 video encoding. Each module is selectable to suit the vehicle and mission profile without disturbing the rest of the stack.