MOST ADVANCED, MOST AFFORDABLE GPS RECEIVERS & SENSORSThe receiver can be used as primary means of navigation during en-route, terminal and LNAV approach phases of flight. It is designed specifically to meet the requirements of TSO-C145c Class Beta 1. It is the enabling technology for several key applications including:

� Primary means of navigation

� En-route, terminal, and LNAV approach phases of flight

� Automatic Dependent Surveillance-Broadcast (ADS-B)

� Constant descent approach

� Current and advanced TAWS

� Advanced ATM

� Required navigation performance enhancements

Affordable GPS-SBAS Receiver for Aircraft Navigation and Approach

NexNav mini™ is a low power, small form factor FAA certifiable GPS-SBAS

receiver with the following features:

� GPS L1 C/A code Sensor card with SBAS capability

� Compatible with WAAS, EGNOS, MSAS and GAGAN

� Certified by FAA for TSO-C145c Class Beta-1 operation

� Suitable for primary means of navigation during en-route, terminal and LNAV phases of flight

� Complying to the latest FAA standard DO-229D

� 12 GPS and 3 SBAS channels

� Receiver Autonomous Integrity Monitoring

� Comprehensive PBIT and CBIT

� Up to 5 Hz update rate

� DO-178B level B and DO-254 Level B design assurance standard

� Fully customizable input/output protocol

� Field loadable software

� Configurable Time mark signal

� Environmental qualification as per DO-160E

NexNav mini has the next generation solution today.

NexNav mini-T™

GNSS SENSOR TECHNOLOGY

Accord Technology LLC

# 26, West Lone Cactus Drive,

Phoenix, Arizona, USA 85027

Tel:

Fax:

www.accord-technology.com

info@accord-technology.com

+1.623.271.8800

+1.623.271.8243

location... location... location...Accord Technology LLC

PERFORMANCE CHARACTERISTICS

Conformity

RTCA

FAA

Performance

General

Number of channels

Hor. Position Accuracy1

Di�erential Position Accuracy1

Vertical Position Accuracy1

Velocity Accuracy1

Time Accuracy1

Update rate

Sensitivity

GPS Tracking

Other Features

ADS-B Support

Altitude Aiding

Approach capability

ENVIRONMENTAL CHARACTERISTICS

Temperature

Altitude

DO-229D, DO-301, DO-228, DO-178B, DO-254, DO-160E

TSO-C145c, Class Beta 1

GPS C/A code Sensor card with SBAS capability

12 GPS and 3 SBAS

5 m, RMS

3 m, RMS

7 m, RMS

0.1 m/s, RMS

30 ns, RMS

5Hz

-145 dBm

Available, as per DO-229D Appendix U

Pressure and baro altitude aiding per DO-229D

LNAV approach

-50˚ to 70˚C

60,000 ft (18,200 m)

Dynamics

Speed, Accelerationand Jerk

Integrity

RAIM

FD/FDE

Alert

BITE

Design Assurance

Hardware

Software

Interfaces

Host interface2 each

Time mark

Messages

Upgrades

ELECTRICAL CHARACTERISTICS

Power Input

Power

PHYSICAL CHARACTERISTICS

Dimension

Weight

RF Connector

I/O Connector

Per DO-229D requirements for en-route, terminal and LNAV approach.

SBAS integrity incorporated

FD/FDE incorporated

Software alert per DO-229D

Comprehensive power-on and online self-tests

Per DO-254, Level C

Per DO-178B, Level C

RS-232 ports

TTL and RS-422

Proprietary messages, NMEA 0183

Software upgrades through serial port

5 .5 Vdc - 28 Vdc

1.8 W

3.5˝ x 3.0˝ x 0.6” (89 x 76.32 x 12.7) mm

1.5 oz. (45 gms)

SMA RF connector, Socket

14 pin dual row, Socket

1 Typical values at 1 Hz and nominal signal strength. Performance speci�cations are subject to GPS system characteristics, U. S. DOD operational degradation, ionospheric and tropospheric conditions, satellite geometry, and multipath e�ects. Assumes SA O�.