BRIEF INTRODUCTION:
1.1 Feed subsystem: Double-offset reflector Gregorian antenna.
1.2 Antenna structure subsystem: Azimuth/Elevation turntable, Feed, support leg and etc.
1.3 Antenna control subsystem: Azimuth/Elevation/Polarization motor, Azimuth/Elevation/Polarization angle sensor, ACU case, controller, etc.
DETAIL:
1. The main support system of the antenna is carbon fiber material. The system realizes 60% carbon fiber, the material is more stable, the weight is lighter, the strength is higher, and it is more convenient for portable use.
2. The antenna has the features of low sidelobe and high gain, which can meet the technical requirements of satellite companies.
3. The antenna system is equipped with GPS positioning system, position detection system, polarization adjustment system, servo drive system, automatic protection system, high performance satellite beacon receiving system, Wi-Fi wireless control, intelligent control management software and so on.
5. Under special circumstances, when GPS can not be used, the satellite longitude and latitude can be input manually, and the pointing can be completed quickly.
6. It provides three automatic and manual control modes to facilitate emergency operation in various environments.
DATASHEET:2.4m Flyaway Carbon Fiber Antenna
2.4m Flyaway Carbon Fiber Antenna Datasheet (Auto)
