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ARINC 743A GPS
Frequency 1575.42 MHz
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S67-1575-52: Same as (-16) except 26 dB gain internal amplifier with
special filtering for airline applications. Requires +4 to +24VDC with
internal voltage regulator. D.C. bias is provided through the coax
connector. Height .55".
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PDFs
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| Model |
ARINC 743A GPS S67-1575-52 |
| Electrical |
 |
| Frequency |
1575.42 MHz |
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| VSWR |
2.0:1 |
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| Polarization |
RHCP |
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| Impedance |
50 OHMS |
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| Antenna Gain (Typ) |
3 dBic @ Zenith |
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| Gain Coverage (min) |
-1.0 dBic 0° ≤ Ø ≤ 75°
-2.5 dBic 75° < Ø ≤ 80°
-4.5 dBic 80° < Ø ≤ 85°
-7.5 dBic Ø = 90° @ Horizon
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| Gain (preamp) |
26.0 dB |
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| Noise Figure |
2.5 dB |
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| Power Handling |
1 watt |
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| Voltage |
+4 to 24 VDC |
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| Current |
25 mA |
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| Lightning Protection |
DC grounded |
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| Mechanical |
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| Weight |
6 oz |
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| Height |
.55" |
| Width |
3.0" |
| Length |
4.70" |
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| Material |
6061-T6 aluminum / thermoset plastic |
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| Finish |
Skydrol resistant enamel |
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| Connector |
TNC |
| Environmental |
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| Temperature |
67°F to +185°F |
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| Vibration |
10 G's |
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| Altitude |
55,000' |
| Federal & Military Specs |
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| FAA TSO |
C115a & C129 |
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DO-160, MIL-STD-810, ARINC 743A,
MIL-C-5541, MIL-E-5400 |
| Model |
GPS S67-1575-20 L1 & GPS S67-1575-39 L1 |
| Electrical |
S67-1575-20 |
S67-1575-39 |
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| Frequency |
1575.42 MHz |
1575.42 MHz |
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| VSWR |
1.5:1 |
2.0:1 |
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| Polarization |
RHCP |
RHCP |
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| Impedance |
50 OHMS |
50 OHMS |
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| Antenna Gain (Typ) |
3 dBic @ Zenith |
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| Gain Coverage (min) |
-1.0 dBic 0° ≤ Ø ≤ 75°
-2.5 dBic 75° ≤ Ø ≤ 80°
-4.5 dBic 80° ≤ Ø ≤ 85°
-7.5 dBic Ø = 90° @ Horizon |
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| Gain (preamp) |
26.0 dB |
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| Noise FIgure |
2.8 dB |
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| Power Handling |
1 watt |
1 watt |
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| Voltage |
+4 to 24 VDC |
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| Current |
25 mA |
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| Lightning Protection |
DC grounded |
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| Mechanical |
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| Weight |
3 oz. |
5 oz |
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| Height |
.40" |
.57" |
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| Width |
3.5" |
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| Material |
6061-T6 aluminum/thermoset plastic |
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| Finish |
Skydrol resistant enamel |
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| Connector |
TNC |
| Environmental |
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| Temperature |
-67°F to +185°F |
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| Vibration |
10 G's |
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| Altitude |
55,000 |
| Federal & Military Specs |
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| FAA TSO |
C115a & C129 |
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DO-160, MIL-STD-810, MIL-C-5541, MIL-E-5400 |
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