Suborbital meteorological rocket "Tobol"
Objectives of the project
Conduct a study of the lower layer of the earth's atmosphere, the troposphere, using a high-precision air temperature and humidity sensor.
Reach the apogee of the rocket's flight path at 1 km above sea level and land at a safe vertical speed of about 5 m / s.
Determine the exact location of the aircraft using GPS coordinates.
The rocket design is based on additive technologies. A damaged part, such as a stabilizer, can be replaced with a 3D printed copy. The aft part is made of carbon fiber, most of the mountings are screw.
High output radio modules allow two-way communication between the command center and the missile.
Аппаратное обеспечение полетного контроллера
Графики изменения основных параметров полета с течением времени