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.

Duratek's power supplies and power distribution units are designed and manufactured to generate and distribute stable electrical power required by equipment, tailored for defense applications in naval, ground, aerospace, and space environments.

MDCX, multipin coax connectors, offer low VSWR of 1.25:1 (typ) up to 10 GHz (max mated pair), maximum overall diameter of 0.125" fitted into low-profile micro-D housing, with constant 50 Ohm airline impedance. MDCX coaxial contacts are compact in size allowing multiple high density connections in a Micro-D style shell for applications where space and weight savings are important. No cumbersome spring mounts are required. These connectors are also available with locking post mechanisms or blindmate hardware attachment.

[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

The first step toward armed helicopters The Bomb Rack Unit (BRU) is a device installed on a helicopter’s Stub-wing to mount various armaments such as rocket launchers and air-to-ground missiles, and it consists of a Pylon Unit and a Bomb Rack Unit. CTLA’s Bomb Rack Unit is equipped with a Boresight function that allows vertical (up/down) and horizontal (left/right) angle adjustments, and a solenoid-actuated free-fall weapon release (Jettison) method is applied. CTLA’s Bomb Rack Unit has passed the system tests for the Light Armed Helicopter (LAH) and received suitability certification, and it is currently in mass production.

L14F type liquid level switches

Dynamic Load Carriage® system Dim. : 6.5" W PALS webbing for MOLLE attachment Patented Ballistic Vein® Composition Material : 500D Cordura® + ARAMID / PV® Size : SMALL 26" - 30" MEDIUM 29" - 33" LARGE 32" - 36" XLARGE 36" - 40" Colors: MC (MultiCam) BMC (Black MultiCam) BK (Black) RG (Ranger Green) CYT (Coyote Brown)

EMCORE’s IPADS-I (International) provides significant enhancements for today’s Army and Marine Corps survey teams. IPADS offers a proven, reliable, lightweight, off-the-shelf solution developed around four main components. > Compact Position/Navigation Unit (CPNU) > Control and Display Unit (CDU) > Battery and Charger Unit (BCU) > Porro Prism Assembly (PPA) All components are housed in a robust frame that allows for easy component access and stability, while facilitating a ready, two-person transfer between vehicles and aircraft. Features High-precision common survey enables efficient mass fires Impervious to jamming (inertial mode) Embedded Selective Availability Anti-Spoofing Module (SAASM) GPS option Navigation aids (compass rose and digital maps) In-vehicle and offset survey Combat-proven Embedded Built-In Test (BIT) High reliability MTBF, low mean time to repair (MTTR) No periodic calibration required Applications Artillery Survey to Mark: Survey Control Point (SCP) position; used to initialize weapon systems Orienting Line (OL) position and azimuth; used to initialize and align artillery assets