The main wheel assembly refers to the complete structural unit that includes the wheel, tire, axle, bearings, and in most cases, the braking system. As the primary load-bearing gear, the assembly is engineered to absorb high-impact forces during landing and provide strong braking performance during deceleration. Its design integrates durability, safety, and serviceability, making it a critical element of aircraft ground operations.

SAS(360° Situation Awareness System) is a day and night multi sensor system, giving the capability of 360 degree’s situational awareness in the battle field. SAS comes with an uncooled thermal camera as well as a day CMOS sensor supplying crew members in the vehicles with the information out of vehicle for better situational awareness. Each SAS camera provides 90° filed of view and up to 360° with more cameras onto the various kinds of vehicle. SAS-PTV(Panoramic Triple Vision) - Single and Duo (PTV-S / PTV-D) is the device that forces can be aware of 360° surrounding situation in the vehicles through It can me mounted onto M1A1/A2, K1A1/A2 and any other vehicles for optimal performance in complete darkness for driver and commander PTV-S or PTV-D with Wide Field of View provides an optimal image quality an situational awareness capability of the forces SAS comes with an uncooled thermal camera as well as a day CMOS sensor supplying crew members in the vehicles with high definition video for better situational awareness.

The ASN-157 was developed to meet the ongoing need for helicopters with reduced size and weight avionics. The ASN-157 system has an accuracy of 0.15 percent of total velocity, weighs less than 13 lbs., consists of one line-replaceable unit, and has a predicted mean time between failure of over 7,300 hours.

Spring probes are designed to optimize performance in high reliability, multicycle applications. Smiths Interconnect’s spring probes are compliant which makes them ideal for blind mate applications as they self correct for x, y, z, rotational and angular misalignment of the target. Offered in compressed heights less than 2 mm and utilized on pitches as tight as 0.4 mm, they are well suited for high density, board-to-board, battery contact and high frequency applications. Mixed signals and functionality can be designed into a single connector.

Antibacterial/FR treated padded spacer mesh system Poly mesh cummerbund for increased ventilation XFrame® Dynamic Load Carrige® compatible Compatible with our entire accessories line Flush admin chest pocket with internal elastic straps PALS webbing for MOLLE attachment Zipper for Assaulter's Zip-On Back Panels QASM buckle system Holds up to five 5.56mm magazines Internal plate pocket retention straps accommodate several different plate thickness Soft armor included Composition Material: 500D Cordura® + ARAMID/PV® Size : Small / Medium : 8.5" x 11.5” -9.3" x 12.3" Plate Pocket Front Panel Area of Coverage : Length 13.25” Width 11" Large / XLarge : 10" x 13"- 10.9" x 13.8” Plate Pocket Front Panel Area of Coverage : Length 15" Width 12" Colors: MC (MultiCam) BMC (Black MultiCam) BK (Black) RG (Ranger Green) CYT (Coyote Brown)

The CAS-500(Compact Advanced Satellite), phase #1 project is the project in which KAI aims to develop a CAS500-1 by operating a joint design team with Korea Aerospace Research Institute(KARI) and to transfer the government’s satellite development technology to the industries. Then, KAI initiates the development of the CAS500-2 project and establish the industry-led development as well as mass-production infrastructure.

- 3 axis Fiber Optic Gyroscopes / 3 axis MEMS Accelerometers - Operating Range: ± 490º/sec - Bias Repeatability(over temp. range) : ≤ 0.5º/hr (1σ, RMS) - In-run Bias Stability: 0.03º/hr (typical, 1σ) ≤ 0.05º/hr (max, 1σ) - Angle Random Walk : 0.025º/√hr (typical, 1σ) - Power Consumption: 5W @ 25℃ (< 8 W, @ - 40℃) - Input Voltage: + 5 V Lightweight Package: 790g (1.74 lbs)