SPRINT

SPRINT is a project that officially began just one month prior to its first hotfire at Launch Canada.

SPRINT's modular architecture supports quick configuration changes, efficient testing, and fast learning. The results of our hotfire puts us on track to flying our flight-weight system now in development.

Subsystems

Propulsion

Feed system, valves, and fluid dynamics for the liquid bipropellant engine. Features pneumatic control architecture with fail-safe valve positions and industry-standard fittings.

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Electrical

Ground support equipment for data acquisition and rocket control. IP65-rated enclosure with LabJack T7-Pro, PLC, and LabVIEW HMI for safe operations.

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Avionics

Flight computer and sensor modules for the 4" rocket system. Custom PCB modules for power, telemetry, recovery, GPS, and sensor acquisition.

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Tests

Hot Fire Test - September 13th & 14th, 2025

Multi-day hot-fire test campaign demonstrating improved engine performance and system reliability across multiple firing sequences.

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Hot Fire Test - August 22nd, 2025

Hot-fire test of the SPRINT system demonstrating successful ignition and combustion.

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Cold Flow Test - August 9th, 2025

Cold-flow test validating fluid dynamics and system integration.

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