InterGravity Technologies has developed a Type-III Composite Overwrapped Pressure Vessel (COPV) optimized for high-performance small spacecraft propulsion systems. The tank is designed with an aluminum alloy liner for impermeability and a carbon fiber/epoxy composite overwrap for high strength-to-weight ratio. The system is tailored for green propellant storage (C₂H₆, N₂O), offering an exceptionally lightweight yet robust solution for orbital transfer vehicles and CubeSat-class platforms. Technical Specifications - Type : Type-III COPV (Al liner + CFRP wrap) - Volume : 5.3 liters - MEOP : 75 bar - Proof : 230 bar - Burst : 250 bar - Dry Mass : < 1.0 kg

Taktic buckle system for quick connect & release 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 DS Assaulter's Zip-On Back Panels QASM buckle system Increased structural integrity and reduced rear deformation 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 SDI170 IMU is designed for demanding, mission-critical, rugged environments and ideal for continuous use applications with no wear-out components, highly linear accelerometer performance and longer life compared to competing alternatives. It is constructed with EMCORE’s latest generation quartz gyros, quartz accelerometers, and high-speed signal processing to achieve outstanding precision performance. The solid-state quartz sensors and hermetically sealed IMU construction provide reliable MTBF and a 20-year operating and storage life. Continuous Built-in Test (BIT), configurable communications protocols, electromagnetic interference (EMI) protection and flexible input power compatibility make the SDI170 IMU easy to use in a wide range of higher-order integrated commercial and defense system applications.

Confronting climate change, designing quieter and more efficient airplanes, developing innovative satellites to observe the Earth's system: our sector is using its skills to their utmost to take action for the environment. Our two main objectives are to advance our technologies so that we can better observe our planet and to create sustainable air travel.

The SBC3612D is a rugged 3U VPX single board computer aligned with the compute-intensive SOSA profile, delivering high-performance processing with the Intel® Xeon® D-2775TE 16-core processor and flexible expansion capabilities. • Supports up to 64GB DDR4 SDRAM and 480GB NAND Flash (NVMe SSD) • Offers 100GbE and 10/25GbE data plane and control plane support • Features the Xilinx® Zynq® UltraScale+™ MPSoC FPGA for enhanced security

The KF-21 is the project which aims to replae the aged fighters in operation, F-4, and F-5 of the Republic of Korea Air Force and develop the indigenous Korean fighter aircraft which is equipped with performances suitable for the future battlefield of the country's air force. Korea's largest-scaled KF-21 project is the national R&D project with a development span of 10 years and 6 months and is driven with Indonesia under international joint development. Based on its development experience and infrastructure of a homegrown airplane, such as the KT-1 basic trainer, T-50 Advanced Jet Trainer, TA-50 Lead-in-Fighter-Trainer, and FA-50 Light Combat Aircraft, KAI is under development of the KF-21 project successfully. Through this project, KAI plans to develop the aerospace technology of Korea and contribute to national peace and security as well as economic development.

NO MELT, NO DRIP (50/50 NYLON COTTON) Incorporate 4-way stretch Tweave (Waist band, knees, Groin) Universal knee pad pockets Mesh and string rubber tip at the bottom to improve convenience Fit adjustment though the Velcro behind the knee and bottom parts to protect body temperature and support agile activity Front low profile, rear and ventilated cargo Pockets Applied MIL-SPEC threads and YKK zippers Composition Material: NYLON 50% / COTTON 50% Size : Waist 28~36, Leg S, R, L Colors MC (MultiCam) BMC (Black MultiCam) BK (Black) RG (Ranger Green) CYT (Coyote Brown)

CarboNIX NEO is an off-the-shelf separation system available in 8", 15", and 24“, 31.6” and 38.81” sizes. It is scalable to any custom diameter for satellites upwards of 1000 kg. While NEO uses the same lock mechanism and pusher arm subsystems as CarboNIX, NEO employs a new clamp ring system which is stronger, stiffer, can withstand higher loads and launch heavier spacecraft than any other separation system on the market.