Recovery

About the team

The recovery team is responsible of the designing, manufacturing and testing the recovery subsystem of our rockets, whose function is to make sure that the vehicle returns to land safely, once its mission has been completed. Some examples of the tasks involved in designing this system are the selection of appropriate parachutes and cordages or the design and testing of the ejectors. Due to its nature, in order to design this system, we need to thoroughly collaborate with other departments, such as Mission Analysis (parachute selection for an appropriate descent rate), Aerostructure (integration of the system inside the fuselage of the vehicle) and Payloads (incorporation of deployable payloads in some of the recovery events).

Highlight Projects

SRAD CO2 EJECTOR
The recovery team has designed a CO2 ejector that provides a pressure source capable of deploying the recovery bays of our vehicles. It makes use of commercially available compressed CO2 canisters as a less energetic alternative to black powder charges, commonly used for rocket recovery.

 The design was validated in Lince’s flight at EuRoC23’, where, despite flying in tandem with a conventional BP charge for redundancy, it successfully triggered the first recovery event. A more sturdy and powerful design revision was developed for use in Pícaro at EuRoC24’, this being our first rocket to deploy using only CO2 ejection.
DUAL DEPLOYMENT
After two years trying to make an “inline recovery system” work without success, the team has decided to switch to a more reliable “dual deployment system” in order to incorporate dual event recovery into our rockets. 

With this system the rocket separates at two different points of the airframe, at different times during descent, releasing the drogue and main parachute at the appropriate altitude.
SRAD SHOCK CORDS
The team is trying to develop their own kevlar cordage to assemble the recovery system. By doing it themselves, they have more control on the lengths and thicknesses of the shock cords, and can design a more optimized and safe recovery system. 

The team will also be testing the mechanical properties of the elements they use in the recovery system.

THE TEAM

BRUNO MORENO
  • PROPULSION
     MARKETING
    AEROSTRUCTURE
    AVIONICS
  • PAYLOADS
    GCS
    MISSION ANALYSYS

PHONE

+34 620 222 539

E-MAIL

contact.star@uc3m.es

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