Nano spacecraft
Nano spacecraft
Nano spacecraft
NANOSATELLITES
GS-1
GS-1
Nanosatellites
DESCRIPTION
GS-1 spacecraft built on the CubeSat class satellite bus was designed mainly to verify in space environment the adopted fundamental engineering solutions to the thruster and test new technologies, components, materials, software to be used in the prospective projects.
SATELLITE BASIC SPECIFICATIONS
| Overall dimensions, mm | 111 × 110 × 370 |
| Mass of the satellite bus, g | 2987 |
| Orbit: | |
| – type | near-circular |
| – altitude, km | 350–800 |
| – inclination, deg | 48–98 |
| Type of propulsion unit | environmental monopropellant |
| Mass of propulsion unit, g | 1000 |
| Total burn of the propulsion unit under test, N·s | 320 |
| Attitude accuracy, deg | 10 |
| Active lifetime, years | >1 |
EARTH REMOTE SENSING SPACECRAFT
GS-1
GS-1
Nanosatellites
DESCRIPTION
GS-1 spacecraft built on the CubeSat class satellite bus was designed mainly to verify in space environment the adopted fundamental engineering solutions to the thruster and test new technologies, components, materials, software to be used in the prospective projects.
SATELLITE BASIC SPECIFICATIONS
| Overall dimensions, mm | 111 × 110 × 370 |
| Mass of the satellite bus, g | 2987 |
| Orbit: | |
| – type | near-circular |
| – altitude, km | 350–800 |
| – inclination, deg | 48–98 |
| Type of propulsion unit | environmental monopropellant |
| Mass of propulsion unit, g | 1000 |
| Total burn of the propulsion unit under test, N·s | 320 |
| Attitude accuracy, deg | 10 |
| Active lifetime, years | >1 |
