The new Super-TAC IMU integrates three fiber optic gyros that exceed tactical grade performance with three high-accuracy Micro-Electro-Mechanical Systems (MEMS) accelerometers and state-of-the-art support electronics in a single small, lightweight package. This solution addresses the need for superior inertial performance in a tactical- grade package, critical for operation in GPS denied and contested environments. The Super-TAC IMU measures change in velocity and angle, utilizing a configurable variable synchronous data link control (SDLC) digital serial bus. The Super-TAC is configured to offer customers the best value solution when designing new systems as well as provide the flexibility to upgrade existing platforms. The Super-TAC IMU employs state-of-the-art optics with fewer components, providing significant performance and reliability improvements across standard military environments. Background Emcore, located in Budd Lake, NJ has been designing, developing and producing inertial components, sensors and navigation systems for Space, Ground, and Avionic applications for over 35 years. Emcore has been developing Fiber Optic Gyros (FOGs) since the early 1990s, producing and delivering IMU products with performance ranging from tactical to strategic grade PERFORMANCE GYRO PERFORMANCE Bias Stability < 0.05 °/hr. (1σ) Angle Random Walk ( ARW) ≤ 0.01 °/√hr. (1σ) Scale Factor Repeatability ≤ 100 ppm (1σ) Scale Factor Linearity ≤ 50 ppm (1σ) Angular Rate Range 1,000 °/sec Acceleration Range 100,000 °/sec2 ACCELEROMETER PERFORMANCE Range ± 25 g Bias Variation ≤ 50 μg (1σ) Scale Factor Stability ≤ 300 ppm (1σ) SYSTEM PERFORMANCE Bandwidth (adjustable) 800 Hz (gyros) 150 Hz (accelerometers) MTBF >25,000 hr.

This miniature fin actuator manufactured by MPS Microsystems was designed based on customer specifications. Designed to guide a very small object and disposing of an extremely limited space, it meets 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.

It is a system that performs missions such as monitoring, surveillance and reconnaissance by ejecting and launching a foldable fixed-wing drone from the canister(tube) launcher. It is equipped with EO/IR Cameras (Electro-Optical / Infra-Red), which are mission equipment for reconnaissance, so that effective day and night image information can be collected. The gathered image information is transmitted to the ground control system (GCS) in real time while detecting and tracking the target by applying AI-based image processing technology. The foldable fixed-wing UAV has a simple structure and light weight, so it can be stored and transported in the canister launcher, and can be operated immediately so that it can be operated without time delay, and if necessary, the air vehicle can be retrieved and re-used by using a net-type recovery system.

Armada is one of the worlds leading defence technology analysis magazines since 1976. The editorial includes technology analysis, information about ongoing procurement programmes worldwide, news analysis, comments and interviews from top defence officials. It has become the go to defence encyclopaedia for the defence community, especially those who make purchasing and procurement decisions.

Monitors abnormal engine operation based on digital and analog signals from the aircraft engine. It calculates engine life indices and detects engine malfunctions for generate a Pilot Fault List (PFL), which will stored in memory. When an engine failure is detected, it provides warning for display on the Central Maintenance Panel (CMP). Developed as a replacement for obsolete, achieving 60% cost competitiveness compared to equivalent products. - x1 MIL-STD-1553B - x16 Discrete Inout - x14 Discrete Output - x3 Analog Input - x1 RS-232 - Size: 283 x 265 x 89 (mm) - Weight : 4.1Kg - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G - Power : MIL-STD-704F (28VDC, 25W)

- To check and verify the RWR system on the aircraft and radiate threat signals to RWR antenna through couplers. - Radiate threat signals to jammer system.

We have taken the standard housing configuration of the P1 & P3 mounting dimensions while incorporating true differential pair contacts within the P1 & P3 dimensional constraints. P1 connector housing contains 21 position true differential pair blind mate contacts allowing board designers to carry high density differential pair signals from the LRU via motherboard to daughter-card plug in modules with a single connector P1 type housing.

Wooribyul Co., Ltd. will continue to develop the best products and solutions using wired/wireless technologies accumulated over a long period of time and provide customized services to customers