Receives vibration signals from an accelerometer installed on the aircraft engine and monitors engine vibration. Processes real-time vibration signals and converts them into IPS AVG units for output. Developed for localization, achieving 50% cost competitiveness compared to equivalent products. - x1 MIL-STD-1553B - x2 UART(RS-422/485) - x2 Accelerometer sensor - Sample rate : Up to 5,000Hz - Size : 220 x 206 x 52 (mm) - Weight : 1.75Kg - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G - Power : MIL-STD-704F (28VDC, 10W)

It is commonly used in industrial and other devices to generate triggers ranging from one to several thousand FPS, ensuring precise timing synchronization with various devices. Periodic Mode: Continuously generates trigger signals after configuration. Burst Mode: Generates a single trigger signal upon receiving the best command via serial communication. *** Product Expansion and Usage ***  Four Operating Modes  Periodic mode: Generates a single-cycle signal based on the configured frequency and duty ratio.  Burst mode: Generates a single-cycle signal synchronized with a software trigger.  External trigger mode: Generates a single-cycle signal synchronized with an external trigger.  External trigger bypass mode: Distributes signals triggered externally.  Connect the trigger output signals from a Master Trigger Generator to a Slave Trigger Generator (as shown below).  By connecting one of the Master TG’s Trigger Outputs (1 to 16) to the Slave TG’s External Trigger Input: Outputs 1 to 15 of the Master TG remain unchanged. Outputs 16 to 31 of the Slave TG will mirror the Master TG’s Trigger Output. (Note: Each trigger signal passing through a TG experiences a delay of ten ns. However, since trigger outputs operate in the range of tens to thousands of Hz, users will not notice the delay).  Example with 17 TGen-16C units: Produces up to 256 Trigger Output Channels (16 × 16).

Orbit’s TT&C ground stations antenna must function flawlessly in order to provide a narrow beam width link in one-time single opportunity, flight test event. Add this factor to the turbulent weather that is often present at the ground station locations, and you are looking at a formidable hurdle. Orbit provides fixed, transportable, and portable antenna systems that feature auto-track, RSSI-track and GPS track tracking modes, unsurpassed tracking accuracy and durability to deliver the stable connection required for dependable data throughput. Our stabilized T&T antenna systems work in extreme temperature conditions (-40°C to 55°C) and in rough weather, for example, at base stations that are close to the ocean or on high mountain ranges.

Aviation piston, cylinder, airplane bolts and nuts Tank engine block , Tank nozzle and cover, single wiper driving unit, Balkan parts, composite wrench, 60mm mortar, 4.2inch mortar, 90mm recoiless rifle, 2.75"rocket warhead, 81mm mortar, target for shooting range

With expertise in manufacturing guidance, navigation, and control (GNC) products, we have been used in over 2,000 spacecraft. Adaptable for size, moment, and power to meet optimal system requirements. Redundant windings available. Current, speed, and torque control. Simple digital interface to the spacecraft bus. Hermetically sealed. Long demonstrated lifetimes. ISO 14644-1 state-of-the-art cleanroom facility. ISO 9001:2015 certified.

Stable operation through precise current/temperature control for up to 4 channels. Customer-tailored GUI, real-time monitoring, and remote control.

The Improved Fire Control System (IFCS) PNU / Universal Fire Control System (UFCS) UPNU family represents a true state-of-the-art system approach. Its design features permit ready adaptation and/or optimization to any current or future weapon system or sensor requiring precision pointing and positioning. The PNU / UPNU and its variants point the way for the future direction of the land navigation systems. Utilizing advanced sensors, electronics, software and aiding (GPS and odometer), the PNU / UPNU family delivers precisely what the Army of tomorrow needs — a system designed to remain operationally effective and affordable to support well into the future. Features High-performance RLG-34 ring laser gyros Common architecture and components (Paladin, PIM, Firefinder, IPADS) Embedded 12-channel Selective Availability Anti-Spoofing Module (SAASM) Impervious to jamming (inertial mode) Resistant to jamming (GPS-aided mode) Combat-proven Embedded Built-In Test (BIT) High reliability MTBF, low mean time to repair (MTTR) No periodic calibration required Applications Multiple Launch Rocket System (MLRS) High-Mobility Artillery Rocket System (HIMARS) Pointing and position location

33 GHz Mixed Signal Oscilloscope; 4 analog / 16 logic channels