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AN-ARN-149V data sheet

AN-ARN-149V data sheet

AN-ARN-149V data sheet

Product catalog summary
Overview
The AN/ARN-149(V) is a low-frequency automatic direction finder designed for military aircraft, providing enhanced navigation capabilities. It features a lightweight design, synthesized digital tuning, and compatibility with MIL-STD-1553B digital multiplex bus, while retaining an analog interface.

Key Features
  • Lightweight system under 11 lbs.
  • Frequency coverage from 100 to 2199.5 kHz in 500 Hz steps.
  • Integrated sense-loop antenna with dual antenna option.
  • Dual identification tone filter for improved Morse code identification.
  • Coherent detection for better adjacent channel rejection.
  • Two preset emergency channels.
  • Easy retrofit using existing control wiring.
  • High reliability with a predicted MTBF of 4,900 hours.
  • Enhanced maintenance with a hinged chassis for easy access.

Operating Features
The system automatically points to low and medium frequency non-directional beacons, standard broadcast stations, and emergency stations. It processes signals from the dual loop and sense antenna, providing bearing information to a radio magnetic indicator or cockpit display unit via the MIL-STD-1553B bus.

System Specifications
  • Modes: Antenna, ADF, Tone, Ident, Test.
  • Frequency range: 100-2199.5 kHz with 500 Hz channel spacing.
  • Receiver sensitivity: 70 µV/M in Antenna mode, 100 µV/M in ADF mode.
  • ADF bearing accuracy: ±3° from 100 µV/M to 0.5 V/M.
  • Power requirements: 27.5 V dc, 0.6 A max with 1553B; 26 V ac, 400 Hz, 0.5 A max.

Physical Specifications
  • Receiver dimensions: 3.15 x 5.04 x 12.00 in.
  • Control dimensions: 5.75 x 2.26 x 3.50 in.
  • Mount dimensions: 3.36 x 1.30 x 13.00 in.
  • Single antenna dimensions: 8.60 x 1.75 x 16.60 in.
  • Dual antenna dimensions: 10.62 x 1.10 x 23.81 in.

Weight
  • Receiver: 5.5 lb with MIL-STD-1553B, 4.7 lb without.
  • Control: 1.6 lb.
  • Mount: 0.35 lb.
  • Single antenna: 3.1 lb.
  • Dual antenna: 5.1 lb.

Qualification
  • Receiver: C41c and DO-142, DO-160A environmental category.
  • Temperature/altitude: -55 to +71°C, sea level to 70,000 ft.
  • Humidity: 95%, 10-day cycle.
  • Vibration and shock specifications per DO-160A standards.

Contact Information
For more information, contact Rockwell Collins at 400 Collins Road NE, Cedar Rapids, Iowa 52498, or via phone at +1.800.321.2223 or +1.319.295.5100.
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Catalog excerpts

AN-ARN-149V data sheet-1

AN/ARN-149(V) low-frequency automatic direction finder Provides enhanced navigation for military aircraft around the world. The Rockwell Collins AN/ARN-149(V) is the first low-frequency automatic direction finder to provide an internal, field-upgradable MIL-STD-1553B digital multiplex bus capability. This system, consisting of a receiver, control, antenna and mount, provides a low-frequency automatic direction finding function in a lightweight, easily installed set. The all solid-state receiver eliminates all moving parts such as goniometers, synchros and mechanical tuners. Quadrantal Error Correction (QEC) is set by aircraft connector strapping, eliminating corrector modules and airframe-specific internal adjustments. The antenna combines the loop and sense antennas and preamplifiers in one compact housing, thereby eliminating expensive sense panels, couplers and special prefabricated cable assemblies. A dual version of the same antenna is also available in one aerodynamic package. The receiver is controlled by a four-wire serial bus from the control. >> Two preset emergency channels >> Easy retrofit; uses existing control wiring in most cases >> Internal QEC, connector-strapped; airframe wiring sets QEC KEY FEATURES >> Lightweight – under 11 lbs for complete system >> Meets RTCA MOPS >> Synthesized digital tuning >> High reliability; predicted MTBF is 4,900 hours >> Internal, field-upgradable, MIL-STD1553B compatibility (input and output functions) with retention of analog interface >> 100 to 2199.5 kHz frequency coverage in 500 Hz steps; positive digital selection >> Integrated sense-loop antenna, dual antenna available for dual installations >> Dual identification tone filter enhances Morse tones for positive aural identification even with noisy reception conditions >> Coherent detection for improved adjacent channel rejection >> DO-160 rated for hard mounting in helicopters and fixed wing aircraft >> Enhanced maintenance; hinged chassis for easy access to modules for fast fault isolation; compatible with existing ADF test equipment >> Design refresh 2011

 Open the catalog to page 1
AN-ARN-149V data sheet-2

operating features The Rockwell Collins AN/ARN-149(V) LF ADF system provides automatic pointing to low and medium frequency non-directional beacons (NDB), standard broadcast stations and emergency stations on frequencies of 500 and 2182 kHz. The frequency is selected in 500 Hz increments on the control, or via the MIL-STD1553B data bus. The receiver processes the signals received from the integrated dual loop and sense antenna and provides bearing information to a standard radio magnetic indicator (RMI) via the 3-wire synchro interface and to either a cockpit display unit (CDU) or an aircraft...

 Open the catalog to page 2

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