Roxel has well-established facilities and experienced staff available for performance testing of a variety of propulsion systems including solid propellant rocket motors, thrusters, hybrid engines and air-breathing systems. These systems can be trialled over a range of conditions to simulate the operating environment and include:
- Static and dynamic
- Operating temperature from –65°C to +80°C
- Simulated flight profile (e.g. aerodynamic heating or high altitude)