Quadro expands the capabilities of Exolaunch's microsatellite separation systems with a four-point offering tailored to match the Arrow 150 satellite with masses up to 250 kg. It is currently the only separation system which is qualified to fly the Arrow 150 platform on the SpaceX Transporter missions. Quadro was crowned the most innovative separation system in Europe by winning the Innovation in Space Award 2023 at the European Space Summit, celebrating its unique blend of flight-proven technology and cutting edge four-point design securing access to orbit for the next generation of microsatellite buses.

Air conditioning units are designed for efficiency, durability, and environmental control, our units help ensure smooth ground handling and turnaround operations in all weather conditions Whether servicing commercial planes or private jets, our units deliver powerful and precise cooling and heating to ensure comfort for passengers and crew.

Low Size, Weight and Power (SWaP) at only 297g. Up to 100 TOPS GPU by NVIDIA® Jetson Orin™ NX Supports multiple camera and sensor interfaces 2x GbE and 2x USB3 for RGB/ Infrared/ hyperspectral cameras and lidar/ radar 2x GMSL2 for HDR/ 3D cameras Built-in UART and CAN to interact with flight controller 1x M.2 2230 for storage and 4G/5G communication ready Supports 4S-14S drone battery pack Compatible GMSL2 cameras with pre-built drivers

Intel® 14th/13th/12th-Gen Core™ 24C/ 32T 35W/ 65W CPU Affordable IP66-rated design for waterproof and dustproof Up to 96GB DDR5 4800 SODIMM -25°C to 70°C wide-temperature fanless operation 3x 2.5Gb and 1x Gb Ethernet ports via M12 X-coded connectors, with 802.3at PoE+ option 1x waterproof USB3.2 Type-C port supporting alternative mode for DisplayPort and USB3.2 dual output 8V to 48V DC input with built-in ignition power control

ICONYX™ is a high-performance tactical grade Inertial Measurement Unit (IMU) for guidance and control applications. ICONYX™ is designed to meet the most demanding environmental conditions with extreme accuracy and reliability. Proven Technology Safran proposes an IMU based on Hemispherical Resonator Gyroscope the HRG Crystal™. This technology is combat proven for 15 years and is extremely accurate, reliable, and is capable of navigating in the most contested GNSS denied environments. HRG Crystal™ Embedded Thanks to the HRG Crystal™, ICONYX™ surpasses the highest performances of its category while keeping the best in class SWaP (Size, Weight, and Power) characteristics of the market. High performance in demanding environments ICONYX™ includes 3 hemispherical resonator gyroscopes HRG Crystal ™ and 3 closed loop MEMS (Micro Electro Mechanical Systems) accelerometers in a compact package. Both Safran’s gyroscopes and Safran’s accelerometers are technological breakthrough.

[LEO GNSS-R] Satellite : LEO RF Characteristics : GPS L1/L5, Galileo E1/E5a(option) Accuracy : Position ≤ 10m(3DRMS), Velocity : ≤ 1m/s Raw Data Accuracy : Pseudo-Range : 1m(RMS) Carrier-Phase : 10mm(RMS) Data Output Rate : 1Hz 1PPS Accuracy : Sync to GPS Time Data < 1us (1PPS Accuracy < 1.5us) TTFF : Cold Start ≤ 20min / Warm Start ≤ 10min Dara Interface : MIL-STD-1553B, RS-422(Data Interface) [GEO GNSS-R] Satellite : GEO RF Characteristics : GPS L1/L2C/L5, Galileo E1 Accuracy : Position :: ≤ 30m(3DRMS), Velocity : ≤ 1m/s Raw Data Accuracy : Pseudo-Range : 1m(RMS) Carrier-Phase : 10mm(RMS) Data Output Rate : 1Hz 1PPS Accuracy : 2us(RMS)/Sync to GPS Time Data TTFF : Cold Start ≤ 45min / Warm Start ≤ 20min Dara Interface : MIL-STD-1553B EEE Parts : ITAR Free Parts

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Type : Axial (3P) Size(Ø, mm) : 230 × 87 Weight(kg) : 14 N. Speed(rpm) : 4500 N. Torque(Nm) : 75(Air)/85(Liquid) N. Power(kW) : 35(Air)/40(Liquid