Rolatube Tripods are purpose-built for applications where mobility, speed, and performance matter. Constructed from Rolatube’s patented rollable composite material, each tripod offers a durable yet lightweight structure that rolls or folds down for easy transport and storage. Designed to support a range of payloads and mission profiles, the lineup includes the highly portable System 30, versatile Industrial Compact Tripod, and robust System 50 Tripod MIL for demanding field operations. These tripods are engineered for rapid deployment and compatible with Rolatube masts or other payloads requiring stable elevation. Their corrosion-resistant build, compact footprint, and tool-free setup make them ideal for communication, surveillance, and sensor support across defence, emergency response, and industrial sectors.

With a peak torque of >200Nm / 1770 lbf-in and a rated torque of 80Nm / 708 lbf-in, the fully redundant DA 58-D is the strongest, electromechanical, fully integrated (actuator control electronics, position sensing, motor and drivetrain in one housing) actuator in the market. Besides the well-proven redundant RS 485 interface, the DA 58-D also features a redundant CAN bus interface. The DA 58-D has been developed for applications with the highest reliability demands. The redundant – two channel – design of the actuator allows continuous operation even if one of the two channels has failed. All major components such as the electric motors, control and communication electronics, and power supply are available twice (redundant). The actuator features a triple-redundant position sensor (2 out of 3 voting). Additionally there are several sensors integrated to provide diagnostic information such as current consumption, supply voltage levels and temperature readings. All major components of the actuator are continuously diagnosed by the microcontrollers of the actuator and its health status can be read via the redundant RS485 / CAN interface.

Product Description and Features 1. Usable Time: Approximately 4 hours 2. Breathable Coolant: Semi-permanent (reusable) 3. Oxygen cylinders and valves: Inspected by the Korea Gas Safety Corporation (KGS) 4. Materials: Outer fabric and PET material are heat-resistant. 5. Drain Button: A device for removing moisture depending on the usage time. 6. Supply Button: A device that temporarily provides a large amount of oxygen. 7. Facepiece: Includes a manual defrost for long-term use. 8. Electronic Pressure Indicator with IT Technology: Life-Saving Alarm (PASS) function, ambient temperature display, container pressure display, automatic alarm for low pressure (approximately 50 bar), usable time display, battery status display, and NFC-based personnel monitoring system (free software provided). 9. Accessories: Bone conduction communication equipment can be applied.

EMCORE’s SDI170 IMU is designed as a performance-compatible inertial system that is form, fit, and functional with a legacy RLG-based IMU product, but with superior overall performance, versatility, and a significantly higher MTBF (Mean Time Before Failure) rating over ruggedized environments. The tactical performance of the SDI170 IMU is based on EMCORE’s mature, proven, dependable and accurate quartz MEMS inertial sensor technology in our SDI500 tactical-grade IMU. EMCORE’s quartz technology enables repeatable high-volume production of precisely machined sensor structures combined with the inherent large signal output and thermal stability of quartz materials. 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.

PBS TJ150 turbojet engine features a compact design and excellent thrust-to-weight ratio. Built-in starter-generator provides reliable starting and power to the deck network. Customisation possible (adjustment of hinges, length of outlet nozzle, etc.) A version of the engine with pyrotechnic ignition is available. A version of the engine is available that allows it to be re-used after a landing in salt water.

The SBIR Training Program prepares business owners to write compelling SBIR/STTR grant applications with state-of-the-art proposal development workshops, structured mentoring, and follow-up guidance from proven business experts. SBIR (Small Business Innovation Research) and STTR (Small Business Technology Transfer) are highly competitive awards-based programs that finance small businesses hoping to commercialize their technology innovations.

It is especially suited for demanding applications, which require reliable performance, such as missile seeker gimbal stabilization, where small size and low power consumption is required, while in a low cost design that is also ideally suited for high volume commercial applications. System Performance PARAMETERS SPECIFICATIONS Standard Ranges ±100°/sec, ±200°/sec, ±400°/sec Input Voltage + and - 5.0 Vdc Bandwidth 110 Hz Output Noise < 005°/sec/√Hz Scale Factor Accuracy ±1% Nominal Features Dual Axis Capabilities in Small Form Factor Miniature Size: Only 25gm.(1.05” x 0.71” diameter) Hermetically Sealed In Stainless Steel Cylinder High Reliability DC Input/High-Level DC Analog Output Low Cost Applications Tank Turret Stabilization Missile Targeting Platform Stabilization Antenna Stabilization Camera Stabilization Spacecraft

Nara Space’s first standard nanosatellite for Earth observation constellations with 7 optical bands and 1.5 m GSD. Launched November 2023 to the 525 km of the orbit, it has 2 years Mission Lifetime.