T-Minus CanSat Launcher
T-Minus Engineering
Reusable, parachute-recovered rocket launcher deploying up to 6 CanSats above 1km altitude.
Technical specifications
- Height
- 3.17 m
- Diameter
- 0.2 m
- Total mass
- ~23 kg
- Motor total impulse
- 4300 Ns
- Burn time
- 4.2 s
- Payload capacity
- up to 6 CanSats
- Recovery
- parachute, reusable
About
The T-Minus CanSat Launcher is a solid-propellant rocket vehicle designed to launch and deploy up to six CanSat-format educational or technology-demonstration payloads to altitudes above 1km. The vehicle is parachute-recovered and reusable across multiple flights, making it well suited for university and STEM CanSat competition programs as well as low-cost payload testing campaigns. It is built by T-Minus Engineering using the same in-house solid propellant manufacturing and mechanical/electrical integration capability used for the company’s DART sounding rocket program.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
