SSKM-R (IRIDIUM) Satellite aircraft tracking system terminal
SSKM-R is designed for transmission of the information about the aircraft location and other aircraft parameters (SSKM-R2), voice communication and exchange of the text messages via Iridium satellite communication channel (SSKM-R1).
Key user benefits:
- Designed according to the United Nations AFF standard;
- Voice communications via iridium satellite system;
- Channel encoding of the transmitted data with 256 bit key;
- Alarm signal entry from control panel;
- Short text message receiving/transmission by control panel
SSKM-R1 - voice and data
SSКМ-Р2 - only data
Specifications
| Parameter | Value |
|---|---|
| Power supply, V | 18 - 30.3 ( DC power supply) |
| Power consumption (Tx/Rx), max | |
| - at temperature higher - 5 °С, max | 7 / 20 |
| - at temperature below - 20 °С, max | 25 |
| Used satellite network | Iridium |
| Data volume in one package, Rx/Tx, bytes | |
| - SSKM-R1 | 1890 / 1960 |
| - SSKM-R2 | 270 / 340 |
| Maximum altitude for operation, m | 15 200 |
| Operating temperature, °С | |
| - АSА-R1 antenna | from - 55 to + 70 |
| - PU-R1 control panel | from - 20 to + 55 |
| - BSPP-R1, R2 transceiver | from - 45 to + 55 |
| Dimensions (WхHхD), mm | |
| - АSА-R1 antenna | 195 х 80 х 50 ( above fuselage) |
| - BSPP-R1, R2 transceiver | 161 х 80 х 45 |
| - PU-R1 control panel | 171 х 65 х 21 |
| Weight, kg | - АSА-R1 antenna |
