CA450Ku-ku band Civil Airborne Satellite Comminication System

CA450Ku-ku band Civil Airborne Satellite Comminication System

Civil Aviation Airborne Satellite Comminication System

Description

 

  Prior to the 1970s, civil aviation aircraft in transoceanic and remote areas can only achieve air-toground communications, air traffic management through short-wave, ultra-short-wave communications, with the introduction of satellite navigation and communication systems, the entire route, and even the worldwide air-to-ground communications and air traffic management services.Aviation satellite communication system can be divided into cockpit satellite communications and cabin satellite communications, the current cockpit satellite communications mainly use the L band, cabin satellite communications mainly use Ka or Ku band.

 

  With the development of satellite manufacturing technology and millimeter wave technology, airborne satellite communication has been developed to the Ka or Ku band, SATPRO's Ka or Ku-band broadband satellite communication system has the advantages of high throughput, low cost, wide coverage, small terminal, etc., can guarantee the high-speed, reliable and real-time transmission of aircraft health data and cabin broadband. Improve aircraft flight safety, implement aircraft failure analysis, improve aircraft dispatch rate, improve aircraft condition monitoring and health management, improve passenger experience, become the future direction of development and market commanding heights.

 

Specification

Electronic specification

Antenna Type

Linear

LHCP/RHCP

Operation Frequency

Rx:10.70~12.75GHz

Tx:13.75~14.50GHz

Receive G/T(Elevation 10°)

12.1dB/K@12.75GHz

Transmit EIRP(dBW)

48.4dBW@14.25GHz

RF Input(Tx) 13.75-14.50GHz,WR62

RF Output(Rx)

950-2150MHz,TNC 50Ω


Mechanical specification

Size

945*260mm

Weight

37kg

Azimuth range

360°continuous rotation

Elevation range

0°~90°(80° peeformance reach the standard)

Az/Ei Velocity:Acceleration

>60°/s,>100°/


Antenna tracking specification

Cross pollsolation

≥25dB(TYP)

Tracking Accuracy

≤0.2°RMS


Other requirements

DC power

DC 28V

Power consumption 120W(average)

Operation temperature

-55°C~70°C

Altitude

16800 meters(55000 feet)

Comply with the standard

ARINC 791-P1   ARINC 791-P2

RTCA DO-160G     RTCA DO-178


KRFU:Ku-band Radio Frequency Unit

ITEMS

Specifications(BUC)

RF Frequency

13.75~14.50GHz

IF Frequency

950-1950MHz

Saturated Output Power

47 dBm(typ.),46 dBm(min.)

Rated Output Power 46 dBm

MOP(Maximum Operational Power

46 dBm

Gain 70 dB nominal,67 dB min
Input Voltage 115VAC,360-800MHz,400Hz nominal,Single Phase
Dimension L558mm*W230mm*H89mm
Weight ≤11kg
Operation Temperature -11~55℃(long time),-40℃~70℃(short time)
Storage Temperature -55℃~85
Environmental Requirements RTCADO-160G
Design Reference Standard ARINC 791

KANDU:Ku-band Aircraft Networking Data Unit

ITEMS

Specifications

Servo Range of Motion

Azimuth:0~360°(continuous)

Pitch:0~90°

TX Polar:0~360°(continuous)

RX Polar:0~360°

Speed of Motion

Azimuth:0~60°/s

Pitch:0~60°/s

TX Polar:0~60°/s

RX Polar:0~60°/s or Electronic adjust

Track accuracy:≤0.2°RMS

Input Voltage

115VAC(97VAC-134VAC),360-800MHz,Single Phase

Input Current 4.3 Amps
Output Voltage(to OAE) +28 VDC
Dimension L450mm*W230mm*H86mm
Weight ≤7kg
Operation Temperature -11~55℃(long time),-40℃~70℃(short time)
Storage Temperature -55℃~85
Environmental Requirements RTCADO-160G
Design Reference Standard ARINC 791

 

Features

 

  KRFU

  The function of KRFU Unit includes receiving the Ku-band or Ka-band satellite signal ,Up-conversion of the Modman IF signal to a Ku-band or Ka-band RF signal use able by the antenna and Power amplification of the Ku-band or Ka-band Block Up-Conversion output.

  KRFU consists of Ku or Ka-band Block Up Converter(BUC),High-Power Amplifier(HPA),Digital detection receiver and AC to DC Power-supply module.

  KANDU

  Ku-band or Ka-band aircraft networking data unit is the main control unit of the system. The functions of the KANDU is including 2 axis servo-stabilization, track satellite, sensor data read, system logic control, protocol process and analysis, GNSS data calculate, etc.

 

Applications

 

Helicopter, civil aircraft, and other airplanes.

 

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