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

An Angle of Attack (AOA) indicator is a flight instrument that shows a pilot the angle between the aircraft's wing and the oncoming air, providing a crucial safety margin by warning of an approaching aerodynamic stall. Unlike airspeed. A Vertical Speed Indicator (VSI), also known as a Rate of Climb and Descent Indicator (RCDI) is an instrument which indicates the rate of climb or descent of an aircraft. These devices are installed and compatible with F-16 series aircraft and KAI's T-50/FA-50 series aircraft.

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

- RWR receiver inspection and antenna performance measurement - EW receiver inspection - Check the azimuth and signal power of the RWR receiver

Mixed Signal Oscilloscope (4) Analog Channels, 10M record length, Certificate of Traceable Calibration Standard

JEFF WRAITH I is the tactical goggle for Military & Law Enforcement. The lightweight goggles give you wide protective coverage with a comfortable fit for use. It is compliant with ANSI Z87.1 standard requirement, European CE standard, and exceed U.S. Military eyewear ballistic resistance requirement MIL-PRF 32432A, MIL-DTL-43511D. The Anti-Scratch & Anti-Fog coated polycarbonate lenses give you up to 99.9 protections form UV rays and you can wear the goggle with your glasses on.

The RFcore Radar series are FMCW type radar and were developed to detect/track small air targets. The major difference between three models is detection performance. RX32B is fundamental model. RX128B have four times larger radar than RX32B. RX192A have six times larger radar then RX32B. The number of the product name means the number of antenna elements. All have compact and lightweight physical architecture that concentrates all the components required for radar, such as antenna, RF components and radar signal processor, in a small single housing. Transport can be carried in the carrier box and can be easily carried by one person. For installation, you can use a commercially available camera tripod. The weight is about 7.5kg (RX32B) and 15.9kg (RX128B), and the lower connection part is compatible with the tripod connection for the camera. Power supply requires 12VDC (RX32B) and 24VDC power (RX128B and RX192A). When using a battery, it is possible to connect a 12V battery or 24V battery to radars. Usage time may vary depending on the battery capacity. RFCORE recommended the constant power supply. Transfer of Status and BIT information and simple control of the RX32B, RX128B and RX192A are possible with a web browser using the Ethernet connection for authorized users. Using the terminal program provided with the radar, you can view the radar control and detected target information in real time. All RX Radar series’ Power Amp and Core Chip were designed using RFcore's own products.

Our radars’ low-Size, Weight, and Power (SWaP) means ample room for other onboard sensors, such as Electro-Optical and Infrared (EO/IR) cameras. Users no longer need to decide which sensor to include and which to exclude. Instead, they can understand the bigger picture. Highly reliable, the NSP-3 has a recommended maintenance interval of 1,250 hours. It can gather data over land and maritime environments and can be used for applications as broad as sea ice monitoring and search and rescue, as well as specialized intelligence, surveillance, and reconnaissance (ISR) missions.