Universal Modular Space Platform C
Platform for small spacecraft weighing up to 700 kg. Height of operation on different types of orbits – from low circular to geostationary. The ICA platform is divided into several independent modules. Each module separately is a subsystem of the platform and is a functionally and structurally separ
Technical specifications
- Working orbits
- Low circular orbit or the geostationary orbit
- Platform weight
- 300 kg for remote sensing and up to 340 kg for MKA communication
- Payload weight
- Up to 300 kg for DZ and up to 260 kg for MKA communication
- Payload power supply capacity
- 400 watts for RS and up to 1500 watts for the ICA connection
- Orientation
- Three-axis, active
- Orientation accuracy, deg
- ±0,08 deg for remote sensing to 0,1 deg for the ICA connection
- Nominal voltage, V
- 27±0,5
About
Platform for small spacecraft weighing up to 700 kg. Height of operation on different types of orbits – from low circular to geostationary. The ICA platform is divided into several independent modules. Each module separately is a subsystem of the platform and is a functionally and structurally separate unit, which has clearly defined mechanical, electrical and thermal interfaces. Stage of development: Manufactured tooling for the Assembly of the platform and the ICA on its basis. The layout of the platform was made and the layout of the platform and the ICA (remote sensing and communication) was carried out on its basis. Made layout for dynamic and acoustic tests. Mechanical and acoustic tests of the platform were successfully carried out. All parameters and characteristics of the platform are confirmed.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.