Applications
- Transponder
- Telephony
- Data Link Subsystem (DLS)
- Drone Flight Control System (DFCS)
A high power, half wavelength, coaxial dipole assembly encased in a fiberglass radome and mechanically structured for aircraft operation. The dipole is used instead of a monopole to increase horizon coverage and requires no ground plane.
| Speed |
Mach 1.2 |
| Altitude |
70,000 ft |
| Temperature |
-54°C to +70°C |
Meets the following requirements of Mil-Std-810:
| Temperature-Humidity-Altitude |
Method 518.01 Proc 1 |
| Shock |
Method 516.2 Proc 1 |
| Vibration |
Method 514.2 Proc 1A |
