Acquire high quality images with accurate radiometry for LEO (Low Earth Observation) earth observation applications with 65 MP focal plane and control electronics. From a 500 km orbit, SEEING™ 230 Ident has 9 x 6 km2 swath, offering a 1.03m native Ground Sample Distance (GSD), and features a super-resolution optional mode providing 70cm GSD. Thanks to its unique design, SEEING™ 230 Ident has an ultra-low SWaP factor. It is made of advanced ceramic material for strength during launch and stability during operation in space. It is athermalized and gradient insensitive between -10°C to +50°C. It has a low mass, below 8kg, saving both platform and launch costs.

The N-CUBE comes as a unique solution that combines GNSS signal processing and RF front-ends. It implements the latest state-of-the-art positioning and synchronization techniques, to reach top class of performances for Real-Time Precise Onboard Orbit Determination (P2OD) and accurate time synchronization.

The B.SAFE is a crash-survivable flight data recording for board defense aviation aircraft and helicopters.

B.SAFE is designed to capture audio, video, and data on a Crash Survivable Memory stored in a rugged and highly compact chassis. You can easily replay the recorded data in a standard PC/Windows® environment using post-mission analysis software.

The VS1410 is a video & data recorder/server packaged in a rugged compact chassis (3.75” x 5.75” x 7.36” / 6.4 lb), for recording on a Removable Memory Module (RMM).

Recorded data can be replayed in a standard PC/Windows® environment, using specific or COTS mission debrief solutions for post mission analysis. In addition, typically for ISR applications, data can be replayed while recording on board.

The ENERTEC™ mission data processing and distribution units offer cost-effective and dependable solutions for acquiring, processing, storing, exploiting, and disseminating field and mission data.

These units are suitable for both manned and unmanned ground, air, and sea vehicles. They undergo rigorous validation and formal qualification testing, adhering to standard test methods such as DO-160 and MIL-STD-810.

WeTrack® stands as a one-of-a-kind service developed, possessed, and operated by Safran Defense & Space, Inc. (formerly Safran Data Systems, Inc.). Leverage its autonomous network of radio frequency (RF) sensors to attain precise orbital positions with high data update rates, enhancing your decision-making capabilities across all orbit scenarios, thanks to our global coverage. With automated sensors for detection and tracking, stay well-informed 24 hour, every day of the year.

Our patented technology, designed for passive satellite emissions reception, provides comprehensive coverage of all orbits, boasting multiple networks deployed in the United States, Europe, and Asia. WeTrack® grants real-time access to information through a secure web portal.

ARES (formerly IRIS) from Safran Defense & Space, Inc. (formerly Safran Data Systems, Inc.) represents the next-gen in transportable antenna systems. Packed in portable cases for easy handling, ARES can be shipped using standard methods and be fully operational in under an hour in the field, standing by to support satellites. Utilizing a reliable pedestal design and a dual-band concentric feed, ARES antenna ensures pinpoint accuracy and top-notch antenna performance. Crafted from standard (LRU) parts, it’s a breeze to maintain and service on-site, guaranteeing maximum uptime for all satellite missions. Combined with the SATCORE combo box (Command/Control modem & high-rate receiver) and the TM MAESTRO Monitoring & Control software, ARES is the all-in-one portable satellite tracking system.

KapCOM (EWC33) is a new generation of transceivers with high performance Telemetry, Tracking & Command (TT&C) service. It is used on OneWeb constellation & is based on the heritage of EWC15 used in key space missions like ROSETTA, DEEP IMPACT, …

The PPS®1350 Hall Effet plasma thruster draws on Safran’s long experience with electric propulsion. It is designed for orbital transfer, station keeping and deorbiting satellites and other spacecraft. In particular, the PPS 1350 was the primary engine on ESA’s lunar probe, Smart-1, launched in 2003 by an Ariane 5 rocket. This mission was completed in September 2006.

The Mission Recorder Cockpit Remote Control Unit is mounted in a cockpit dashboard and connect to a recorder system. The MCRCR shows status information on the NVG compatible display and can remote control the Mission Recorder System. 

The ENERTEC™ mission data processing and distribution units are dependable, cost-effective solutions designed to facilitate field and mission data handling, processing, storage, analysis, and distribution. These units are compatible with both manned and unmanned ground, air, and sea vehicles, offering a dependable resource. Each unit undergoes rigorous testing and validation, adhering to industry-standard testing procedures such as DO-160 and MIL-STD-810.