Every year, about 2,500 satellites are launched for navigation, monitoring, and communication missions. Launch costs remain between $10,000 – $60,000 per kilogram, depending on the launch vehicle. Traditional solar panels are heavy (up to 1,500 kg) and rely on complex multi-hinge mechanisms, which often fail in orbit. According to study of deployable structure failures, 55% of all spacecraft deployment anomalies in the last 5 years were caused by solar array deployment malfunctions. CubeSats are cheaper but limited to low orbits due to low onboard energy (less than 100 W typically). These limitations significantly increase mission costs and risks, motivating the development of new lightweight, frameless deployment technologies for CubeSat-class satellites. Our team purpose is to develop a reliable frameless deployable structure for flexible solar arrays suitable for CubeSat platforms to increase the energy level.

korpus cubsata, krepleniye, Bobina, ykladka, patented ydladka, takie-to paneli, piro patron, deploy, centrifuge forces, engines to sustain, algorithm, mcu

Weight -100 Energy +100 Reliability +100 Competitors = Sosyt

Vse krytitsya vertitsya.

email: parasolar@nadosdelat.com