The Mission
Conceived as a “Baptism of Fire”, this mission was the starting point for Cosmic Research. The goal was to gain vital experience in the main subsystems of a rocket: fuselage, engine, electronics and recovery.
The campaign was designed to achieve Level 1 and Level 2 certifications from the Tripoli Rocketry Association (TRA), establishing the legal and technical foundations for the association’s future projects.
It was based on the construction and launch of a commercial kit, specifically the AGM-33 Pike model from the Madcow Rocketry brand.
Beyond the technical aspect, this mission began the tradition of naming rockets after female astronauts to pay tribute to them.
The Rocket
ROCKET LENGTH
OUTER DIAMETER
LIFT-OFF WEIGHT
- Parameter
- Maximum velocity
- Apogee
- Recovery system
- Electronics
- Flight 1 – L1
- ~0.3 Mach
- ~300 m
- Simple Parachute
- None
- Flight 2 – L2
- ~0.6 Mach
- 900 m
- Drogue + Main Parachute
- Redundant flight computers
Propulsion
Valentina utilized an Aerotech H-148R for its first flight and a J-350W for its second.
Recovery
The Valentina recovery system was designed to ensure the safe return of components depending on engine power.
On the first flight, the rocket had a single deployment with a single parachute.
For the second flight, a dual deployment system was implemented to reduce lateral drift during descent. This configuration consisted of a drogue parachute, which was released at apogee, and a main parachute, programmed to open at a height of 150 meters above the ground.
Avionics
Building on the mechanical success of the first launch, the second one introduced a sophisticated electronic flight management system.
This setup featured dual redundancy, combining in-house innovation with commercial hardware to monitor flight progress and ensure the safe, automated deployment of the recovery systems.



