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| Description | Handbook |
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Distributors | Technical Data |
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The navtec EPIRB is a lightweight, portable emergency transmitter for aeronautical and maritime use. It operates in conjunction with the geo-stationary Inmarsat satellites and guarantees rapid transmission of position information in the event of an accident. Four satellites cover about 97 % of the earth's surface. Only one satellite is required for satisfactory operation and three of the four satellites can be reached from Europe at any time. This guarantees that the distress call is forwarded without delay and minimizes the probability of data loss during transmission. A remote control unit (RCU) is available. |
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The navtec EPIRB global-3 can be used as a stand-alone unit without a cradle. In this case only a manual activation is possible. |
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The picture shows the switch and its protection against unintended use. |
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The cradle with the hydrostatic release mechanism can be purchased together with the beacon or later if needed. |
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The navtec EPIRB global-3 can be fitted with an optional Remote Control Unit (RCU). Using the RCU the type of emergency can be specified. The RCU outputs GPS position on its display and its NMEA output. Click on the photo to get an enlarged view (30 kByte). |
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Download a 21 second video-clip from our download page and see worldwide for the first time, how an EPIRB (global-3) is released in 4m depth using the hydrostatic release unit. |
In the maritime version the navtec EPIRB comes as a floating buoy. In case of an accident it automatically ejects from its cradle, surfaces and transmits a distress signal. The navtec EPIRB can also be activated by remote control from a ship's bridge. Furthermore, it can be taken along as a separate unit and activated manually.
In the event of an emergency, the navtec
EPIRB automatically transmits data via the satellites to the base stations.
This data contains the unique EPIRBs system code ()serial number), the
nature of distress, the last position with the actual time as well as the
direction in which the vehicle is moving and its speed. An elaborate CRC
defect protection guarantees transmission and decoding even in case of
disturbances on the transmission path. Tests have shown that all base stations
can receive the signals even with only 100 mW transmission power (1/10
of the nominal transmission power).
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| type | Inmarsat-E |
| Inmarsat type approval number
SOLAS / GMDSS type approval number |
IE-08
0735-00 (wheelmark sign) |
| housing measures (in mm), see figure | 220 high x 210 (diameter) |
| weight | < 1200 g |
| material | polycarbonate |
| maintenance interval/change of battery | 4 years (IMO regulation) |
| maintenance interval of the water pressure ejection in the holder | 2 years (IMO regulation) |
| ejection methods |
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| ejection level (depth) | 1,5 to 4m |
| primary frequencies | 667 channels, 300 Hz spacing from 1,645 GHz |
| type of modulation | carrier-FSK |
| transmission power at the antenna, EPIRB | 30 dBm = 1 W |
| secondary frequency, optional beacon (ELT) | 121,5 MHz |
| type of modulation | AM / A9 / LF sweep |
| transmission power, beacon | 17 dBm = 50 mW |
| frequency error | < 50 ppm |
| integrated flash | red, ca. 2 cd,
ca. 30 flashes/min. increased flash rate during transmission |
| velocity | 2g to 50 Hz, all axes |
| temperature range | 253 ... 328 K (-20 to +55 oC) |
| test function | self test with checking of all functions |
| period of transmission after triggering | min. 48h |
| range, operational range | world-wide, except polar caps, 97% of earth's surface |
| position finding, acquisition time | GPS-RX, 12-channel, cold start 40-100 seconds (!) |
| period of time between triggering and alarming | 3-10 min |
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