Catalog excerpts
Micro-Electro-Mechanical System (MEMS) technology provides extremely precise digital output Reliable: DO-178B, Level A software. Lightweight: 3 component product suite is less than 1.5 lbs. Rugged: Meets RTCA/DO-160E environmental standards. Compact: 2”x 2.5”x 3.9” (ADAHRS). Greater precision The digital Air Data and solid-state Attitude/Heading Reference System (ADAHRS) from Genesys Aerosystems is lightweight and compact. It incorporates a Magnetic Sensing Unit (MSU) and separate Outside Air Temperature (OAT) Probe. This highly accurate system employs the latest Micro-Electro-Mechanical System (MEMS) technology to provide extremely precise digital output and referencing of aircraft position rate, vector, and acceleration da
Open the catalog to page 1
Copyright © 2014 Genesys Aerosystems. All rights reserved. ADAHRS Micro-Electro-Mechanical System (MEMS) technology provides extremely precise digital output ADAHRS Specifications MTBF: 13,000 hrs. (MIL-HDBK 217) COM Ports: AHRS RS232, 19,200 bps. AHRS ARINC-429 (high speed, labels 320, 324, 325, 326, 327, 330, 331, 332, 333 and 377, SDI set by software) ADC RS232, 19,200 bps. ADC ARINC-429 (low speed, labels 203, 205, 206, 210, 211, 212 and 377, SDI set by software) Connector Type: Velocity Accuracy: Meets or exceeds TSO-C106 from 50 to 450 KIAS ±5.0KIAS above 450KIAS Altitude Range:...
Open the catalog to page 2All Genesys Aerosystems catalogs and technical brochures
-
HeliSAS for R66 + R442 Pages
-
HeliSAS for R442 Pages
-
GPS-WAAS Receiver2 Pages
-
S-TEC 5000 Digital Autopilot4 Pages
-
Remote Bugs Panel2 Pages
-
System 60-2 Autopilot2 Pages
-
System 55X Autopilot2 Pages
-
System 40/50 Autopilot2 Pages
-
System 30 ALT & 60 PSS2 Pages
-
SA-2002 Pages
-
ST-3602 Pages
-
GPS Steering2 Pages
-
Yaw Damper2 Pages
-
IDU-680 & IDU-450 EFIS4 Pages
-
HeliSAS4 Pages
-
Integrated Display Units4 Pages
-
System 40/502 Pages
-
IntelliFlight 21002 Pages
-
S-TEC 50004 Pages
