The Transmit/Receive Module splits 2 transmit input channels into 32 output channels. Each channel delivers an output power of at least 3.2 W with a transmit efficiency of 35.5% or higher. It features independent phase control for each transmit channel. On the receive side, 32 input channels are combined into two output channels. The total receive gain is 34 dB or greater, and each channel supports individual gain and phase control. The noise figure is 3.5 dB or lower per channel. Built-in monitoring functions include internal temperature monitoring and output signal monitoring.

The IntuVue RDR-7000 is fully automatic and does'nt require active pilot adjustments of tilt and/or gain for operation. Reducing workload, allows pilots to focus on flying the most comfortable and safest route through weather. Engineered to provide far superior reliability, accuracy and durability than legacy magnetron-based radar systems, the RDR-7000 offers customers the flexibility to remotely enable advanced software features to provide them the clearest view of weather conditions around the routes they’re accustomed to flying. Key Honeywell Advantages: Next generation -fully automated, higher resolution weather radar system with airborne ground/sea mapping system Reliable and efficient - solid-state transmitters utilizing pulse compression provide reduced weight and power consumption, advanced coherent processing, and increased reliability Compact and easy to install - RDR-7000 IntuVue radar systems technology integrated into a small, lightweight package Available software upgrades - advanced features can be added at any time, including turbulence detection, advanced mapping, target detection and additional hazard features (lightning and hail detection), and forward looking (predictive) windshear Honeywell's RDR 7000 Radar helps in operational costs savings by reducing the delays & downtime caused due to hailstorm, weather incidents and windshears while optimizing routes to reduce diversions and turnbacks.

• Band Width : L1/L5 or L1/L2 • Supported GNSS Constellations : GPS/Galileo/NavIC/GLONASS/BeiDou • Interference resistance : - Single jammer interference resistance up to 90 dB(J/S) - Multiple jammers interference resistance up to 82 dB(J/S) - Support of up to 3 jammers simultaneously for each of frequency bands • Interfaces : Digital output • Power Consumption : Low power consumption

The lightest plate carrier 4-way stretch Tweave sewn internally for comfort Poly mesh cummerbund for increased ventilation Rear internal pocket for storage Elastic webbing straps for cable management PALS webbing for MOLLE attachment Removable front flap Zipper for DS Assaulter's Zip-On Back Panels QASM buckle System Available in different shapes depends on the plate thickness Soft armor can be added Composition Material : 500D Cordura® + ARAMID / PV® Size : Small : 8.5" x 11.5" Plate Pocket Medium : 9.3" x 12.3" Plate Pocket Large : 10" x 13" Plate Pocket XLarge : 10.9" x 13.8" Plate Pocket Colors: MC (MultiCam) BMC (Black MultiCam) BK (Black) RG (Ranger Green) CYT (Coyote Brown)

The IMX-5™ includes Attitude Heading Reference System (AHRS) sensor fusion to estimate roll, pitch, and heading. Adding GNSS input to the IMX-5 enables onboard Inertial Navigation System (INS) sensor fusion for roll, pitch, heading, velocity, and position. Features Tactical Grade IMU Gyro: 1.5 °/hr Bias Instability, 0.16 °/√hr ARW Accel: 19 µg Bias Instability, 0.02 m/s/√hr VRW 0.04° Dynamic Roll/Pitch 0.13° Dynamic Heading Surface Mount Reflowable (PCB Module) Fast Integration with SDK and Example Software Data Logging (SDK and Application Software)

This Control Actuation System (CAS) is a guidance system for unmanned flying objects. It consists of three MPS fin actuators that each independently position an aerodynamic fin. The maximum angle of incidence is ±8°, which allows the device to carry out highly precise dynamic manoeuvres. The miniature fin actuators that make up this Control Actuation System are manufactured by MPS Microsystems and were designed based on customer specifications. Designed to guide a very small object and disposing of an extremely limited space, these fin actuators meet strict requirements in terms of performance, weight - less than 100 g - and dimensions. To reduce the length of this actuator, MPS Microsystems used part of the screw length as the motor axis. This screw is equipped with a very compact 4-point contact bearing that simultaneously absorbs axial and radial loads. The angular play on the aileron axis is less than 0.1° rms. This actuator meets the storage and vibration requirements of military equipment.

Military actions today depend on effective use of the electromagnetic spectrum to surveil and assess the battlespace, to protect friendly forces and equipment, and to attack the enemy. That is today's Electronic Warfare (EW), and maintaining a technological advantage across the electromagnetic spectrum can mean the difference between whether or not you complete your missions and bring your forces home.

[LEO GNSS-R] Satellite : LEO RF Characteristics : GPS L1/L5, Galileo E1/E5a(option) Accuracy : Position ≤ 10m(3DRMS), Velocity : ≤ 1m/s Raw Data Accuracy : Pseudo-Range : 1m(RMS) Carrier-Phase : 10mm(RMS) Data Output Rate : 1Hz 1PPS Accuracy : Sync to GPS Time Data < 1us (1PPS Accuracy < 1.5us) TTFF : Cold Start ≤ 20min / Warm Start ≤ 10min Dara Interface : MIL-STD-1553B, RS-422(Data Interface) [GEO GNSS-R] Satellite : GEO RF Characteristics : GPS L1/L2C/L5, Galileo E1 Accuracy : Position :: ≤ 30m(3DRMS), Velocity : ≤ 1m/s Raw Data Accuracy : Pseudo-Range : 1m(RMS) Carrier-Phase : 10mm(RMS) Data Output Rate : 1Hz 1PPS Accuracy : 2us(RMS)/Sync to GPS Time Data TTFF : Cold Start ≤ 45min / Warm Start ≤ 20min Dara Interface : MIL-STD-1553B EEE Parts : ITAR Free Parts