Proof of concept

  • Ultrasonic sensor speed measurement
  • Accelerometer acceleration measurement

Prototype test

Demonstrator test

  • On all gantry and flight tests, the objective of dangerous failure probability (DFT λ) of less than 1*10-3 at 95% is reached, well below that of manual ejection.
  • A study on the flight site, shows a rate of bad assembly of emergency parachutes in harnesses between 5 and 10%. The security gain is well above 100.
  • In addition, the possibility of manual ejection is preserved.