We have experience in developing subsystems for rockets and satellites. We design components to the most demanding specifications.

Our rocket subsystem and component design portfolio:

Pyrotechnic devices

• Pyrotechnic knives
• linear cumulative charges
• pyro valves
• igniters
• servo motors
• followers
• mortars

Rocket recovery systems

• Parachute systems
• wind tunnel testing
• use of flat corkscrew effect
• drop tests
• simulations
• system of recovery from sea surface.

Control and electronic systems for rockets

• On-board computers
• launch management systems
• data acquisition
• control systems

Separation mechanisms

• Auxiliary engine separation systems
• rocket main body separation system
• Łukasiewicz Research Network-Institute of Aviation has successfully demonstrated the following separation methods:
  • „Fire in the hole”,
  • pyrotechnic separation
  • aerodynamic separation.