Project Cavour

Name and design

Camillo Benso, Count of Cavour, was one of the leading figures of the Italian Unification and the main promoter of Italy’s industrial and scientific development. He was born in Turin in 1810, and died in Turin in 1861, being the first prime minister of Italy. PoliTo Rocket Team's first project is named after him.

In accord with the Team's Mission & Vision, Cavour's design is simple and pragmatic, thought to draw the way for future projects. It is also the first rocket of the Founding Fathers series.

Technical characteristics

Cavour is a single stage rocket with a solid COTS motor and an internal diameter of 100mm (3.94in), with a variable target altitude.

It is composed of two body tubes and a coupler, and of four compartments plus the nose cone. The structure is made of lightweight composite materials, and all its internal components are high-performance 3D-printed carbon-reinforced polymers. Starting from the bottom, the rocket’s compartments are:

  • Motor bay, holding the COTS solid motor;
  • Avionics bay with the electronics and the telemetry system;
  • Payload bay, containing with the mission’s scientific payload;
  • Recovery bay, which contains the parachutes and the other recovery components;
  • Nose cone.

  • Cost-effective
    and durable

    Cavour is the first rocket of the Team, and it must be proven that with the least possible budget the group is capable of designing and manufacturing a durable rocket which can sustain a high-powered flight while fulfilling the mission objectives.

  • Reconfigurable

    The Cavour Rocket structure design is modular, able to mount different motors, of different classes, lengths and diameters. Multiple versions of the rocket can be launched with different mission objectives, such as different apogee targets, payload launch and deployment, or system testing.

  • Reusable

    Using a drogue chute and a main parachute, the rocket is designed to land without inflicting any damage to its airframe or to the environment. This allows the rocket to perform multiple launches without inflicting any damage to its airframe or to the environment, so that the rocket is capable of being flown again without any major repair after just some refueling.

Models

CVR 100-75-3
Diameter 0 mmLength 0 mmOperating empty weight 0.0 kgWet mass 0.0 kgPayload 4kg (scientific) Motor model CTI L1350 Liftoff Thrust-Weight ratio 0.0 Maximum thrust 0.0 NMaximum speed 0 m/sTarget apogee 0 m

Launch History

Test Launch

April 29, 2023

On Saturday, April 29th, our Cavour rocket was successfully launched for the first time from a launch site in Bavaria, Germany.

Due to the launch site apogee limitation, Cavour had to be launched with a small and less powerful K-class COTS CTI solid motor, that provided a maximum thrust of 1120.8N. The rocket reached an apogee of 1331.2m, staying under the launch site vertical limit. Cavour flew with a maximum velocity of 162.7 m/s, around Mach 0.5, with a maximum boost acceleration of 9.79G.

The drogue pilot parachute was deployed at apogee, while the main parachute was deployed at high altitudes earlier than anticipated probably due to the malfunctioning of a COTS TD-2 tether, which will be investigated. The rocket descended to the ground with a velocity of 6.9 m/s and landed softly on the German green grass. Cavour landed at around 1.2km from the launch site and was found in perfect condition with all airframe components intact: it is now ready to be reused.

Spaceport America Cup

June 22, 2023

On Thursday, June 22nd, with moderate wind conditions, the Cavour rocket was launched from launchpad B2 of the Vertical Launch Area of Spaceport America, the world's first commercial spaceport located in the Jornada del Muerto desert, approximately 90km from Las Cruces.

The launch was a success, and the rocket reached an apogee of 3142.8m AGL, with a maximum velocity of around 295.4 m/s and a maximum boost acceleration of 17.3G. The apogee was very close to the target apogee (3048m) and to the simulated one. The flight proceeded under nominal conditions, except for an early deployment of the main parachute. This minor malfunction in the recovery subsystem simply drifted the rocket away and did not compromise the integrity of the rocket in any way, as it can be reused for a new launch.

Despite having only one year of experience and being at the first participation in a competition, the Team ranked 20th overall out of the 119 participating universities and 13th in the 10k ft apogee AGL with COTS propulsion category.

Project Cavour won the Dr. Gil Moore Award for Innovation, which recognises a team whose project includes one or more genuinely “novel” or “inventive” features. Project Cavour won this award thanks to the presented extended abstract "3D-printed multilayered fins for flutter suppression", which the judging panel stated stands to revolutionise the industry of rocketry.

European Rocketry Challenge

October 13, 2023

On Friday, October 13rd, at 14:45 (UTC+1), Cavour rocket was launched for the 3rd time in this year from the launch rail at Santa Margarida Military Camp, Portugal.

Cavour completed the boost and coast phase nominally, reaching an apogee of about 2800m with a maximum speed of 266m/s and a maximum acceleration of 14G. After this phase, Cavour descended hitting the ground at 75m/s, due to an undefined failure of one of the rocket's systems.

Overall, Cavour's mission at EuRoC ‘23 was a success, being able to fly again and acquiring an incredible amount of knowledge, skills and experience. This launch set the first of many records for the team, which in minimal time managed to complete two missions at the most ambitious international rocketry competitions.

Project Cavour won the ANACOM "Best Telemetry Spectral Signature" Award, which honors the team with the best telemetry spectral signature. Furthermore, the PoliTo Rocket Team placed 8th in the general ranking among the 25 selected teams, part of the much larger number of applicants.

PoliTo Rocket Team ™ 2024