The Mission
New Christa is an improved version of the original Christa rocket, designed to offer better reusability and reliability.
The main objective of the mission is to act as a launcher for CanSats, with the capacity to carry up to 6 payloads (CanSats) per launch, housed in a gondola system during ascent.
This first launch will serve to validate its operational performance and certify the rocket for use in future European Space Agency (ESA) CanSat competitions.
The Rocket
ROCKET LENGTH
OUTER DIAMETER
LIFT-OFF WEIGHT
ESTIMATED APOGEE
Propulsion
The thrust comes from a commercial solid-propellant motor from Cesaroni Technology. The motor provides a burn time of 1.7 seconds with a maximum thrust of 937.3 N, supplying all the energy needed to complete the planned trajectory.
Structures
The structure uses a high-density design to optimise aerodynamic stability, which is complemented by four symmetrical fins and a boat-tail.
Recovery
New Christa was designed with a dual redundacy design to ensure safe deployment:
- A drogue parachute deployed at apogee
- A main parachute deployed at 150 meters above the ground
Avionics
New Christa features its own SRAD avionics system called Lovelace (in honor to first programmer in history Ada Lovelace), integrated into a custom board that centralises all rocket management.
Reads all necessary data such as acceleration and altitude and stores it in a flash card and a FDR to ensure data storage.
Additionally, the main microprocessor is capable of processing the sensor data, automatically detecting apogee and activating the separation of the rocket that initiate the deployment of the recovery system.
Reliability and optimisation
The New Christa’s design takes a leap forward in robustness and engineering. Significant redundancy improvements have been integrated into critical systems to ensure the safe deployment of the parachutes.
In parallel, we have simplified its manufacture to the utmost, reducing construction complexity to achieve a much more efficient, practical and easy-to-use rocket on the launch pad.




