BioLab Flight Unit
Pressurized biological payload with active chamber sensing, telemetry firmware, and sample exposure control.
Multiple systems are in build, integration, or test. Public technical pages are released after hardware and validation records are ready.
Pressurized biological payload with active chamber sensing, telemetry firmware, and sample exposure control.
Custom flight computer architecture with redundant inertial sensing, deterministic firmware, and data logging.
Long-range telemetry reception, packet parsing, field logs, and live mission visualization.
Terrain-adaptive chassis with modular payload bay, motor control, and embedded navigation under test.
Atmospheric, inertial, and biological sensing routed through I2C and SPI data pipelines.
Guidance, navigation, and control stack for a CanSat-derived satellite platform with simulation-in-loop validation.