LNA/FILTER/COMBINER OMT PRODUCTS
L1 Combiner and LNA
Designed to combine and amplify L1 antennas with pre-filter
The input ports can be increased
GPS and Glonass
Excellent out-of-band rejection
Excellent gain
Superior noise figure
Low current consuption
High 1 dB input compression point
Missile and Airborne Applications
Durable to harsh environmental conditions
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L1 Combiner and LNA |
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|---|---|
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ELECTRICAL |
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| Frequency | 1560-1610 GHz |
| Gain | 29 dB |
| Noise Figure | max 4.8 dB |
| Combiner | 2 input 1 output (3 input 1 output can be optionally) |
| Passband Ripple | ±4 dB |
| Out of Band Rejection | < 70 dBc @1500 MHz <70 dBc @1650 MHz |
VSWR | 2:1 | Input and Output Impedance | 50 ohm | Connectors | SMA (Female) | Max RF Input | -15.5 dBm | DC Supply | 3.3 V (via RF output connector) | Current Consumption | 15 mA (via RF output connector) |
| MECHANICAL | |
| Weight | 22 g |
| Operating Temperature | -40° to +85°C |
| ENVIRONMENTAL AND FUNCTIONAL TESTS | |
| Low Temperature | MIL-STD-810G Method 502.5 Procedure-1 and Procedure-2 |
| High Temperature | MIL-STD-810G Method 501.5 Procedure-1 and Procedure-2 |
| Temperature Shock | MIL-STD-810G Method 503.4 Procedure-2 |
| Low Pressure | MIL-STD-810G Method 500.5 Procedure-1 |
| Acceleration | MIL-STD-810G Method 513.6 Procedure-2 |
| Mechanic Shock | MIL-STD-810F Method 516.6 Procedure-1 |
| Humidity | MIL-STD-810G Method 507.5 |
| Vibration | MIL-STD-810G Method 514.7 Procedure-1 |
L1 Combiner and LNA
Designed to combine and amplify L1 antennas with pre-filter
The input ports can be increased
GPS and Glonass
Excellent out-of-band rejection
Excellent gain
Superior noise figure
Low current consuption
High 1 dB input compression point
Missile and Airborne Applications
Durable to harsh environmental conditions
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L1 Combiner and LNA |
|
|---|---|
|
ELECTRICAL |
|
| Frequency | 1560-1610 GHz |
| Gain | 24 dB |
| Noise Figure | max 7 dB |
| Combiner | 3 input 1 output |
| Passband Ripple | ±4 dB |
| Out of Band Rejection | < 70 dBc @1500 MHz <70 dBc @1650 MHz |
VSWR | 2:1 | Input and Output Impedance | 50 ohm | Connectors | SMA (Female) | Max RF Input | -15.5 dBm | DC Supply | 3.3 V (via RF output connector) | Current Consumption | 17 mA |
| MECHANICAL | |
| Weigt | 30 g |
| Operating Temperature | -40° to + 85°C |
| ENVIRONMENTAL AND FUNCTIONAL TESTS | |
| Low Temperature | MIL-STD-810G Method 502.5 Procedure-1 and Procedure-2 |
| High Temperature | MIL-STD-810G Method 501.5 Procedure-1 and Procedure-2 |
| Temperature Shock | MIL-STD-810G Method 503.4 Procedure-2 |
| Low Pressure | MIL-STD-810G Method 500.5 Procedure-1 |
| Acceleration | MIL-STD-810G Method 513.6 Procedure-2 |
| Mechanic Shock | MIL-STD-810G Method 516.6 Procedure-1 |
| Humidity | MIL-STD-810G Method 507.5 |
| Vibration | MIL-STD-810G Method 514.7 Procedure-1 |
Ka Band Transmit Reject Filter
Features
Compact Design
Low insertion loss
High Rejection
Robust construction
Applications
Dual Polarized Radar Antennas
SOTM Antennas
Vsat Antennas
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Ka Band Transmit Reject Filter |
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TRF Technical Specification |
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| Pass Band Frequency | 19.7 - 20.2 GHz |
| Reject Band Frequency | 25 - 31 GHz |
| Polarity | Linear |
| Return Loss | < 15 dB |
| Insertion Loss | < 0.3 dB |
| Rejection | < 25 dB @25 GHz < 40 dB @30 GHz |
| Flange for connections | WR42 |
| MECHANICAL | |
| Weight | 40 g |
| Operating Temperature | -40° to + 85°C |
| ENVIRONMENTAL AND FUNCTIONAL TESTS | |
| Low Temperature | MIL-STD-810F Method 502.4 Procedure-1 |
| High Temperature | MIL-STD-810F Method 501.4 Procedure-1 |
| Temperature Shock | MIL-STD-810F Method 503.4 Procedure-1 |
| Low Pressure | MIL-STD-810F Method 500.4 Procedure-1 |
| Acceleration | MIL-STD-810F Method 513.5 Procedure-2 |
| Mechanic Shock | MIL-STD-810F Method 516.5 Procedure-1 |
| Humidity | MIL-STD-810F Method 507.4 |
| Vibration | MIL-STD-810F Method 514.5 Procedure-1 |
Ku Band Orthomode Transducer
Features
Compact Design
Low insertion loss
High Isolation
Broadband operation
Robust construction
Applications
Dual Polarized Radar Antennas
SOTM Antennas
Vsat Antennas
Diplexer for Communication Links
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Ku Band Orthomode Transducer |
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|---|---|
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OMT Technical Specification |
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| Tx Frequency | 13.75 – 14.5 GHz |
| Rx Frequency | 10.75 – 12.75 GHz |
| Polarity | Linear, 2 pol |
| Return Loss | < 15 dB @Rx < 25 dB @Tx |
| Insertion Loss | < 0.1 dB @Rx < 0.1 dB @Tx |
| Flange for connections | WR75 @ Rx WR75 @ Tx |
| Isolation | < 55 dB |
| Cross Polarization | < 55 dB |
| MECHANICAL | Weight | 200 gr |
| Operating Temperature | -40° to + 85°C |
| ENVIRONMENTAL AND FUNCTIONAL TESTS | |
| Low Temperature | MIL-STD-810F Method 502.4 Procedure-1 |
| High Temperature | MIL-STD-810F Method 501.4 Procedure-1 |
| Temperature Shock | MIL-STD-810F Method 503.4 Procedure-1 |
| Low Pressure | MIL-STD-810F Method 500.4 Procedure-1 |
| Acceleration | MIL-STD-810F Method 513.5 Procedure-2 |
| Mechanic Shock | MIL-STD-810F Method 516.5 Procedure-1 |
| Humidity | MIL-STD-810F Method 507.4 |
| Vibration | MIL-STD-810F Method 514.5 Procedure-1 |
Ka Band Orthomode Transducer
Features
Compact Design
Low insertion loss
High Rejection
Robust construction
Applications
Dual Polarized Radar Antennas
SOTM Antennas
Vsat Antennas
Diplexer for Communication Links
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Ka Band Orthomode Transducer |
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|---|---|
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OMT Technical Specification |
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| Tx Frequency | 29-30 GHz |
| Rx Frequency | 19.2 – 20.2 GHz |
| Polarity | Linear, 2 pol |
| Return Loss | < 15 dB @Rx < 20 dB @Tx |
| Insertion Loss | < 0.15 dB @Rx < 0.1 dB @Tx |
| Flange for connections | WR42 @ Rx WR28 @ Tx |
| Isolation | < 30 dB |
| Cross Polarization | < 30 dB |
| MECHANICAL | |
| Weight | 100 gr |
| Operating Temperature | -40° to + 85°C |
| ENVIRONMENTAL AND FUNCTIONAL TESTS | |
| Low Temperature | MIL-STD-810F Method 502.4 Procedure-1 |
| High Temperature | MIL-STD-810F Method 501.4 Procedure-1 |
| Temperature Shock | MIL-STD-810F Method 503.4 Procedure-1 |
| Low Pressure | MIL-STD-810F Method 500.4 Procedure-1 |
| Acceleration | MIL-STD-810F Method 513.5 Procedure-2 |
| Mechanic Shock | MIL-STD-810F Method 516.5 Procedure-1 |
| Humidity | MIL-STD-810F Method 507.4 |
| Vibration | MIL-STD-810F Method 514.5 Procedure-1 |