To guarantee maximum safety and reliability, our DA 30 features a brushless motor and a contactless wear-free position sensor. This means maximum service life with the greatest‐possible power delivery and its design prevents electromagnetic emissions (EMI) caused by brush sparking. The housing made of saltwater‐resistant aluminum is HART‐coat treated, meets the IP‐67 standard for water and dust sealing and provides an integrated Sub‐D connector (MIL spec. circular connector or cable gland on request). Brackets integrated in the housing for horizontal and vertical assembly. 8‐fold, ball‐bearing supported, steel gear train, drive shaft with ANSI multi‐tooth. The DA 30 series can be equipped with a standard PWM input (Pulse Width Modulation) that has two different interfaces: a differential, galvanic isolated interface (Opto‐Coupler) and a single‐ended interface with CMOS levels that is also used to program the servo parameters. It includes analog position feedback to detect the drive shaft position. A differential RS‐422 PWM interface can be chosen instead of the opto‐coupled interface. The DA 30 with digital serial command interface (RS‐485) receives its commands via a CRC secured protocol. It can return not only the shaft position in digital format, but also several diagnostic data such as the level of the supply voltage, current consumption and the temperature of the motor and electronics in digital form (optionally also the humidity within the actuator case). These kind of diagnostic capabilities help to determine the health state of the actuators before, during and after deployment.

FOSTEC optical fiber pin/socket terminals are designed to connect to each other through physical contact. POSTECH's unique alignment technology maximizes optical performance and provides reliability.

ICONYX™ is a high-performance tactical grade Inertial Measurement Unit (IMU) for guidance and control applications. ICONYX™ is designed to meet the most demanding environmental conditions with extreme accuracy and reliability. Proven Technology Safran proposes an IMU based on Hemispherical Resonator Gyroscope the HRG Crystal™. This technology is combat proven for 15 years and is extremely accurate, reliable, and is capable of navigating in the most contested GNSS denied environments. HRG Crystal™ Embedded Thanks to the HRG Crystal™, ICONYX™ surpasses the highest performances of its category while keeping the best in class SWaP (Size, Weight, and Power) characteristics of the market. High performance in demanding environments ICONYX™ includes 3 hemispherical resonator gyroscopes HRG Crystal ™ and 3 closed loop MEMS (Micro Electro Mechanical Systems) accelerometers in a compact package. Both Safran’s gyroscopes and Safran’s accelerometers are technological breakthrough.

MQ-9B SkyGuardian® is the next generation of remotely piloted
aircraft systems (RPAS), delivering persistent intelligence,
surveillance, and reconnaissance (ISR) around the globe.
SkyGuardian is designed to fly over the horizon via satellite for up
to 40 hours in all types of weather and safely integrate into civil
airspace, enabling joint forces and civil authorities to deliver real-time
situational awareness anywhere in the world—day or night. Featuring
a longer wingspan than its predecessors at 79 ft (24 m), the aircraft is
outfitted with the revolutionary Lynx® Multi-mode Radar, an advanced
electro-optical/infrared (EO/IR) sensor, and automatic takeoff and
landing capability. In addition to its industry-leading endurance and
superior surveillance capabilities, SkyGuardian seamlessly integrates
with its users’ other platforms, systems, and podded technologies,
dramatically expanding the aircraft's multi-domain mission set

Auto Assembly Jig For : Wing Bottom Panel A320 Project 50m (L) x 1.1m (W) x 3.6m (H )

A gimbal housing is a component that stabilizes and rotates the seeker of a guided weapon. It helps ensure the seeker can accurately aim at the target at all times, regardless of the guided weapon's movement.

InterGravity Technologies has developed a 20 Newton-class bipropellant thruster designed for orbital transfer vehicles (OTVs), lunar hoppers, and micro-spacecraft requiring high efficiency, reliability, and reusability. The thruster operates with green propellants (C₂H₆, N₂O), providing both environmental compatibility and storability advantages. Key Features -Thrust Level : 20N -Specific Impulse : > 295s in vacuum

A ground control system that establishes unmanned aerial vehicle missions, controls aircraft and mission equipment, reads image information, and transmits it to higher-level units.