Proprietary Space Platform
We use Leo-Tugs maneuvering through a sequence of alternating active and passive flight phases.
To increase the orbit altitude, angular orientation and stabilization, the system orients the thrust vector of the propulsion system in the orbital plane close to its velocity vector.
The tug’s mass
94 kg
Maximal payload mass
mPL = 200 kg
Thrust
P = 200 N
Specific impulse
IS = 290 s
Maximum change of the orbit inclination
0,60
Time of the altitude rise from 500 to 600 km
12000 sec
Maximal orbit
1400 km
Max number of propulsion system ignitions
up to 24
Key Project Elements
- Innovative cubesat bus
- Space-proven on-board computer
- Secure software development
- Integration of the satellite with sensing, air/maritime traffic control equipment, ground segment and mission control center
- System operation and capacity distribution among Customers