Transparent transmission navigation equipment multi mode links satellite navigation device
- Category: Aviation Parts & Accessories >>>
- Supplier: Shenyang Shenlan Aviation Technology Co. Ltd.
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Product Overview
Description
Products Description
Place of Origin: | China |
Name | Aircraft satellite transparent transmission navigation equipment(Itype ） |
Material | aluminum |
Color | black |
Function
a. The airborne terminal of the aircraft wide-area monitoring system has independent sensors and multi-mode links. It can
be used independently and can also be crosslinked, it only need to provide the installation location on the aircraft for
independent use, that is: crosslinking with the airborne computer when crosslinking, while sending independent sensor information,receiving on-board computer information and send it to the ground station, but also receive the control order of the groundstation and passed it to the onboard computer;
b. The airborne terminal has the information sensing function of aircraft position,altitude, speed and attitude;
c. The airborne terminal has the function of 4G and satellite dual-mode transmission; It can realizewide-area data transmission and reception, and support data upstream/downstream transmission:
d. Independent power supply, notcrosslinked with aircraft (Type I terminal)
Technical specifications
a.Terminal weight: 230g without antenna; 390g with antenna;
b.Size (without antenna): length: 100mm: width: 75mm; Height: 20mm;
c.Transceiver cycle: 3 to 5 seconds
d.Data service: 1.2Kbps-9.6Kbps
e.Working frequency band: 1980MHz~2200MHz
f.transmission distance: unlimited;
g.Power consumption: 3.5W
h.Maximum transmit power:33.5±0.5dBm;
i.Reception sensitivity: -125dBm@2.4Kbps;
j.EVM:＜6%;
k.Support wide range voltage 9V-36V power supply;
a. The airborne terminal of the aircraft wide-area monitoring system has independent sensors and multi-mode links. It can
be used independently and can also be crosslinked, it only need to provide the installation location on the aircraft for
independent use, that is: crosslinking with the airborne computer when crosslinking, while sending independent sensor information,receiving on-board computer information and send it to the ground station, but also receive the control order of the groundstation and passed it to the onboard computer;
b. The airborne terminal has the information sensing function of aircraft position,altitude, speed and attitude;
c. The airborne terminal has the function of 4G and satellite dual-mode transmission; It can realizewide-area data transmission and reception, and support data upstream/downstream transmission:
d. Independent power supply, notcrosslinked with aircraft (Type I terminal)
Technical specifications
a.Terminal weight: 230g without antenna; 390g with antenna;
b.Size (without antenna): length: 100mm: width: 75mm; Height: 20mm;
c.Transceiver cycle: 3 to 5 seconds
d.Data service: 1.2Kbps-9.6Kbps
e.Working frequency band: 1980MHz~2200MHz
f.transmission distance: unlimited;
g.Power consumption: 3.5W
h.Maximum transmit power:33.5±0.5dBm;
i.Reception sensitivity: -125dBm@2.4Kbps;
j.EVM:＜6%;
k.Support wide range voltage 9V-36V power supply;
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