Manual Deployer of Pico and Nanosatellites
Device for manual start-up of pico and nanosatellites from International Space Station (ISS). Supplied with remote control. There is an option to develop and supply a launch device for automatic launch in any orbit.
Technical specifications
- Working orbits
- Low
- Mass of device
- 3,47 kg ±10% (without thruster), 3,99 kg ±10% (with thruster)
- Mass of payload
- up to 5 kg
- Volume of payload
- up to 100 х 125 х 314 mm
- Linear separation velocity
- 0,25 до 0,50 m/s
- The angular velocity in the separation
- ≤2 deg./s
- Trigger trigger actuation force (remote control keys)
- 2,5 (3) kg
- Overrall dimensions
- 400 х 435 х 160 mm
About
Device for manual start-up of pico and nanosatellites from International Space Station (ISS). Supplied with remote control. There is an option to develop and supply a launch device for automatic launch in any orbit.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.