Mission Description

0480-EX-CN-2018 Text Documents

Raytheon IDS

2018-06-19ELS_211567

KRFS Experimental License Request

1 Purpose of Operation
Raytheon Integrated Defense Systems (IDS) to KRFS Multi-Function RF System
(Radar). This application is to demonstrate this system as a Unmanned Platform. This
will be demonstrated in McKinney ,Texas and Fullerton, California
- File Number: 0480-EX-CN-2018
- Class of Station: FX
- Station Locations: FIXED
- Effective: 07/16/2018
- Expiration: 07/16/2018
Note: The KRFS is designed to operate over specific frequency ranges within the range
of 15.71 to 17.71 GHz. Specific operating modes are confined to the specific bands as
follows:
- 15.71 to 17.71 GHz Radar: C-RAM
- 15.71 to 17.71 GHz Missile Illumination

2 STA Explanation
As detailed in paragraph 1 above, Raytheon seeks this STA in order to allow testing and
technical demonstrations of the KRFS System (Radar).
3. The modulation techniques per mode are listed in the table below.

Mode Modulation PRF Pulsewidth Modulation Rate
Radar : C-RAM Pulse. Bi-Phase or 5 KHz – 200 0.2 – 40.0 usec 20 MHz
Polyphase KHz
Missile Illumination FSK 33Hz 2.5 ms
160 KHz
(Transmit only) Fc ± 1.44 MHz
(Mark)
Fc ± 0.8 MHz
(Space)
Fc ± 1.12 MHz
(Clear)

The peak and mean power per mode are listed in the table below. Because the antenna
is an AESA, the peak power levels are specified at the external face of the radome but
do not include the antenna gain.

Mode Peak Power (Block MaxTX Duty Mean Power (Block 19a)
19b) Cycle
Radar: C-RAM 5760 Watts 20% 1152 Watts
Missile Illumination 1440 Watts 100% 1440 Watts

4. Stop Buzzer
John F. Adams (803)318-0021 Office (714)262-5019 Cell

Document Created: 2018-06-19 17:01:09
Document Modified: 2018-06-19 17:01:09

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