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.
See the complete MACH test timeline
Systems
Propulsion
Feed-system plumbing, ground-support equipment, and quick-disconnect testing.
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Tests
Hot Fire Test - December 15th & 16th, 2025
One cold-weather hot fire reached 510.0 N and 107.2 psi; residual fuel ignited during purge.
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Cold Flow Test - November 20th, 2025
Mission-control integration exposed a wrong V5 mapping, an incompletely installed P4 sensor and a leaking CO₂ fitting.
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Cold Flow Test - November 7th, 2025
Two cold flows followed the control-software rewrite and recorded complete oxidizer-pressure and tank-mass files.
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Hot Fire Test - September 13th & 14th, 2025
Three successful fires; the final run reached 839.1 N, 184.1 psi chamber pressure and approximately 2.4 kN·s.
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Hot Fire Test - August 22nd, 2025
The first SPRINT hot fire reached commanded cutoff, but a partial fill and missing telemetry prevented a measured performance result.
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Cold Flow Test - August 9th, 2025
CO₂ and distilled water flowed after two leak checks passed; an igniter integration failure blocked the planned hot fire.
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