Solid Propellant Motor and General Information
SOMA uses M840 Cesaroni and M2245 Cesaroni solid rocket motors. It is designed to ensure reliable performance during high-altitude flights.
The main objective of the rocket is to collect high-altitude flight data and record sensor data during descent using advanced avionics systems.
Mechanical Features
The rocket body and fins have a trapezoidal structure. The body is manufactured using high-strength composite materials.
Controlled descent is achieved using the Separation System.
A dual-stage parachute system is used, consisting of a Drogue Chute and a Main Chute. The main parachute opens at a certain altitude to ensure a controlled descent.
