Programmes
Four programmes: a sounding rocket, a fixed-wing VTOL UAV, a flight computer and a bench wind tunnel. The avionics are designed and built in house.
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High power rocket
Experimental launch vehicle designed for iterative mission testing, data collection and avionics reliability across flight campaigns. V1 to V4 were static engineering prototypes and were never flown; V5 carries their changes and is the first of the series built to fly.
| Airframe | 2.4 m × 140 mm |
|---|---|
| Dry mass | 9 kg |
| Propulsion | Solid, M impulse |
| Stage | Ground tests complete |
UAV
Fixed-wing VTOL platform for extended atmospheric data collection, aerial imaging and autonomous mission profiling over remote terrain. Nothing has been built yet.
| Configuration | Fixed-wing VTOL |
|---|---|
| Airframe | Composite |
| Endurance | Not yet specified |
| Stage | Pre-prototyping |
Avionics
High power rocket flight computer with three pyro channels, equally usable for model rocketry. Telemetry, onboard control logic and campaign data logging, through hardware-in-the-loop bench validation. It is the avionics package Lynxrocket V5 will fly.
| Processor | STM32H563RIT6 |
|---|---|
| Logging | 16 MB flash at 50 Hz |
| Telemetry | 433 / 868 MHz LoRa |
| Stage | Bench validated |
Test bench
Bench-scale wind tunnel for flow visualisation, built for teaching and demonstration. A 1.29 m duct with a bellmouth intake, run from custom boards.
| Test section | 70 × 200 mm |
|---|---|
| Overall length | 1.29 m |
| Flow range | 10–40 km/h |
| Control | Onboard web server |
Contact
Later Lynxrocket campaigns carry scientific payloads for companies and partners. Tell us what you need to measure.
LYNXSPACE