PRODUCTS

Type

One-button deploy with fully-automatic satellite acquisition, peaking, and cross-pol adjustment using GPS, compass, and level sensors inputs, certified for auto-commissioning on certain satellite systems; one-button stow.

Operator Interface

GUI Interface Program via CFE computer for manual/jog Operation or reprogramming user/data satellite

Auto Positioning Accuracy

≤±0.1 degree

Input Power Requirements

24VDC, 2 amps peak, optional 90-256V AC power supply

Optional
Standard
Rack Mounted
Input Power Requirements
 

Power Supply with handheld operator interface
Two Cases 6 x 6 x 3.5 in (15 x 15 x 9 cm)
1RU Chassis 8 in (20 cm) deep, Wt.3.75 lbs (1.7kg)
90-256V AC, 5 amps peak
 

Reflector

90cm x 66 cm Elliptical

Optics

Offset, Prime Focus

Reflector Construction

Segmented Carbon Fiber

Az/El/Pol Drive System

Patented Roto-Lok® 3-Axis Positioner

Mount Geometry

Elevation over Azimuth

Polarization Alignment

Rotation of reflector/feed aligns major axis with orbital arc

Case Options

Carry-on Suitcase, Rugged Shipping, or Backpack

Controller

One-button Auto-Acquisition

Travel:

Azimuth

180°

Elevation

True elevation readout from calibrated inclinometer

Mechanical

15° to 75° of Reflector Boresight

Polarization

Motorized ±75° with manual H/V selection

Speed:

Slewing/Deploying

10°/second in azimuth, 5°/sec. elevation, 5°/sec polarization

Peaking

0.2°/second

Motors

24V DC variable speed with optical encoders

RF Interface

           RX

L-band with Type -N at rear of antenna

           TX

Ku with Type-N at feed flange

Weight

40-50 lbs. (18-23 kg) depending on case option selected

Stowed Size

Carry-on suitcase/cabin baggage

Manual Operation

Handcranks on all axii