The nose wheel assembly refers to the complete integrated unit consisting of the wheel, tire, axle, bearings, and associated structural components. In some configurations, it also includes steering mechanisms, shock absorbers (oleo strut), and braking systems (for specific aircraft types). The assembly is engineered for durability, precision, and reliability, enabling the aircraft to safely absorb impact forces during landing and provide accurate steering during taxiing.

1. Filler Metal Name Material/Alloy AWS W-No. ISO-No. Nickel 61 Ni A5.14 ERNi-1 2.4155 SiNi2061 MONEL® 60 Ni-Cu A5.14 ERNiCu-7 2.4377 SNi4060 MONEL® 67 Cu-Ni A5.7 ERCuNi 2.8037 SCu7158 INCONEL® 72 Ni-Cr A5.14 ERNiCr-4 SNi6071 NC 80/20 Ni-Cr 2.4639 INCONEL® 82 Ni-Cr A5.14 ERNiCr-3 2.4806 SNi6082 INCONEL® 622 Ni-Cr-Mo A5.14 ERNiCrMo-10 SNi6022 INCONEL® 625 Ni-Cr-Mo A5.14 ERNiCrMo-3 2.4831 SNi6625 INCO-WELD® 686-CPT Ni-Cr-Mo A5.14 ERNiCrMo-14 SNi6686 INCO-WELD® 725NDUR Ni-Cr-Mo A5.14 ERNiCrMo-15 SNi7725 INCO-WELD® C-276 Ni-Cr-Mo A5.14 ERNiCrMo-4 2.4886 SNi6276 INCONEL® 52 Ni-Cr-Fe A5.14 ERNiCrFe-7 SNi6052 INCONEL® 52M Ni-Cr-Fe A5.14 ERNiCrFe-7A INCONEL® 92 Ni-Cr-Fe A5.14 ERNiCrFe-6 SNi7092 INCONEL® 617 Ni-Cr-Co-Mo A5.14 ERNiCrCoMo-1 2.4627 SNi6617 NILO® CF36 Ni-Fe INCOLOY® 65 Ni-Fe-Cr A5.14 ERNiFeCr-1 SNi8065 INCONEL® 718 Ni-Fe-Cr A5.14 ERNiFeCr-2 2.4667 SNi7718 Titanium Grade 1 Ti A5.16-90 ERTi-1 Titanium Grade 2 Ti A5.16-90 ERTi-2 Titanium Grade 5 Ti-Al-V A5.16-90 ERTi-5 Titanium Grade 7 Ti-Pd A5.16-90 ERTi-7 2. Electrodes Name Material/Alloy AWS W-No. ISO-No. Nickel 141 Ni A5.11 ENi-1 2.4156 ENi2061 MONEL® 190 Ni-Cu A5.11 ENiCu-7 2.4366 ENi4060 MONEL® 187 Cu-Ni A5.6 ECuNi 2.0838 ECu7158 INCO-WELD® A Ni-Cr-Fe A5.11 ENiCrFe-2 2.4805 ENi6092 INCONEL® 152 Ni-Cr-Fe A5.11 ENiCrFe-7 ENi6152 INCONEL® 182 Ni-Cr-Fe A5.11 ENiCrFe-3 2.4807 ENi6182 INCONEL® 112 Ni-Cr-Mo A5.11 ENiCrMo-3 2.4621 ENi6625 INCONEL® 122 Ni-Cr-Mo A5.11 ENiCrMo-10 ENi6022 INCO-WELD® C-276 Ni-Cr-Mo A5.11 ERNiCrMo-4 2.4887 ENi6276 INCO-WELD® 686CPT Ni-Cr-Mo A5.11 ERNiCrMo-14 ENi6686 INCONEL® 117 Ni-Cr-Co-Mo A5.11 ERNiCrCoMo-1 2.4628 ENi6617

Cooled thermal imaging camera module F/#4.0 • Detector type: Cooled InSb 15μm (640 x 512) • NETD: <20mk typical (without lens) • Continuous ZOOM LENS • Continuous Digital Zoom • Advanced image processing - Auto Gain Control (AGC) ) - Adaptive Histogram Equalization (Adaptive HEQ) - Local Area Enhancement (LAE) - Digital Detail Enhancement (DDE) - Denoise Reduction (DNR) - Sharpness • MTTF (Mean Time To Failure) 15,000 hours • Various color sets (WhiteHot / Rainbow / Twilight / TwilightShifted / Turbo / Iron / Plasma)

Whether satellites, spacecraft or space debris – GESTRA, the "German Experimental Surveillance and Tracking Radar", is a state-of-the-art radar system for observing and tracking objects in space. It operates in the microwave range and explores the Low Earth Orbit of 300 to 3,000 kilometres, i.e. the range in which most satellites and the International Space Station (ISS) are located. This makes it possible, for example, to protect space systems or the ISS from a collision with debris particles by providing a timely warning. Millions of tiny particles orbit the earth and, at a speed of around 28,000 km/h, pose a threat to active space technologies. GESTRA was developed and built by the Fraunhofer Institute for High Frequency Physics and Radar Techniques FHR on behalf of the German Space Agency at DLR.

The member companies of GIFAS employ 195,000 people in their aerospace activities in France. These figures do not include temporary workers or the total number of suppliers and subcontractors; this field is estimated to be responsible for 350,000 jobs in France. Our sector is constantly in demand.

GAIN CRITICAL CLARITY WITH SATELLITE TASKING Task ICEYE SAR satellites to access groundbreaking data on any location on Earth – day or night and in any weather. The process is simple and images are usually delivered within 24 to 48 hours of your initial request. ORDERING SAR DATA – MADE SIMPLE We believe access to reliable and timely SAR Earth observation data should be available to all, so we provide access options designed to meet your specific mission needs and collection timeframes. The process begins with defining your area of interest, revisit frequency and other parameters. The first images are usually acquired, downlinked, decoded and processed within 24 hours of the initial request and delivered within 8 hours after that.

Integrated Soldier Power / Data Hubs are Personal Area Network (PAN) hub and interconnect systems providing network data access, peripheral connectivity and smart battery power management for dismounted soldier C4ISR electronics in Digitally Aided Close Air Support (DACAS) missions, including precision targeting, tactical radio communications, real-time video downlink, night vision technologies, GPS/navigation, blue force tracking, personal computing and smart phone integration.