MIL-DTL-26482 seriesⅡ has the same contact arrangement as MIL-DTL-26482 series I, and the bayonnet coupling method is applied. The connection between the contact and the wire is a crimping method, which is different from 26482-I. It provides reliable fastening with 5 guide keys. It also has excellent EMI shielding ability and can be used with various additional parts of the M85049 standard, so it is applied to aviation, space, and various high-tech precision equipment.

From start to finish, you will be working with some of the brightest RF engineers and dedicated business professionals in the industry to ensure our antennas deliver the functionality you require. Haigh-Farr will customize a solution for you based on your unique needs while leveraging existing designs to keep costs and cycle time to a minimum.

We manufacture and supply Solar Powered Insect Trap which is and effective solutions for insect control in crop fields. This cutting edge device identifies the Pest and Insects pattern and develops Pest Management and control plan accordingly. Our Solar Powered Insect Trap is very easy to install and operate. Solar Insect Trap offered by us is completely automatic, economical and eco-friendly device. The most advanced Ultra violet luring light secure increased capturing rate than the normal blue LED or fluorescent light in the market In addition, state of the art LED luring light offers virtually unlimited life span unlike the traditional black fluorescent light

Digital mission engineering tools connect every stage of the engineering product lifecycle, from initial design to operation. They enable reality-based 3D simulation across multi-domain environments such as air, space, land, and sea by incorporating high-resolution terrain, satellite orbits, RF and radar systems, and sensor environments to accurately replicate real mission conditions. With accurate dynamics-based physical models at the core, these tools provide quantitative analysis of relative positioning between systems, changes in altitude and attitude, line-of-sight availability, and communication link status. Users can predict and evaluate mission elements such as sensor operations, communication links, platform maneuvers, and orbit optimization through scenario-based simulations.

APA-110 is designed to eliminate CO2 emissions with its unique technical characteristics. It can perform the complete service of aircraft at remote parking places with diesel engine and it is also capable to operate from the 50/60Hz, 400V, 3 phase main power supply grid as any electrical GPU, without fuel consumption and with zero operating emissions. The range of different APA configurations with no emissions allow for safer, cleaner and more practical operational conditions for operators and personnel at the location.

This rocket nozzle featuring conformal cooling channels and isogrid ribbing was manufactured using EOS Copper CuCP, a pure copper material optimized for additive manufacturing. The production required approximately 72 hours, taking advantage of the exceptional thermal and electrical conductivity of pure copper to meet demanding aerospace performance requirements. As one of the few companies in Korea capable of performing metal additive manufacturing with pure copper, we provide advanced technical expertise and support OEM production as well as collaborative technology development projects with various industrial partners. The showcased component was designed by nTopology and demonstrates the synergy of advanced design optimization with state-of-the-art copper additive manufacturing.

Between Earth and space: stratosphere-compatible, solar-powered high-altitude aircraft, known as HAPs (High Altitude Platforms), offer a sustainable alternative to satellites for Earth observation and communication. They are reusable, cost-effective and flexible in use. The DLR joint project HAP-alpha is developing such a technology demonstrator and is endeavoring to establish a complete system capable of permanent operation. The aim is for DLR to build up comprehensive expertise for the development of high-performance, high-flying solar aircraft and to play an active role in shaping the legal framework. In summer 2025, the HAP-alpha successfully passed a ground vibration test.

Consists of a Data Transmission and Recording Unit (DTRU) for data transmission and collection, and a Removable Mass Memory (RMM) for data storage. Stores pre-planned flight mission data in the RMM on the ground and transmits it to the aircraft via the DTRU. Collects various mission data (flight data, monitoring data, video data, and audio data) during flight, stores it in the RMM, and transmits it to the ground for mission analysis. - x5 ARINC-818 Recording as H.264 - x2 Analog audio recording - x7 MIL-STD-1553B Bus Monitoring - x2 Gigabit Ethernet Monitoring - 512GB Solid-State Disk (up to 2TB) - Size : 160.1x146.0x232.4 mm - Weight : 4.25Kg - Power : MIL-STD-704F (28VDC, 58W) - Environment: MIL-STD-810G - EMI/EMC: MIL-STD-461G