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 LEGION 400 tackles the new challenges of the space industry, offering enhanced connectivity, faster delivery, improved value, and unrivaled flexibility.  This antenna system is designed to meet the demands of Earth Observation satellite tracking and the high-volume needs of Communication Satellite Constellations.  What sets the LEGION 400 apart is its patented tri-band S/X/Ka concentric feed paired with a sleek and ultra-precise pedestal. It’s equipped to support LEOP & Launch Vehicles with its cutting-edge S-band Single Channel Monopulse auto track feed.

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 N-SPHERE comes as a new generation of GNSS receiver. 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.

N-XONOS is a X-band transmitter dedicated to small satellites and designed to answer to an increasing demand of high data rate transmission. It is a new generation of transmitters on an innovative design.

The NS1310 is a robust, compact data server and storage unit specifically designed for the challenging conditions of airborne environments. This versatile system functions as a Network Attached Storage (NAS) unit and is equipped with a high-capacity Removable Memory Module (RMM).

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 PPS®5000, produced by Safran Spacecraft Propulsion, is a Hall Effect Thruster purposely designed for “all-electric” satellites. It can operate in high-thrust or high specific impulse mode,and offers an operating lifespan of about 20,000 hours. This means it can handle orbital positioning and station-keeping duties for a wide range of telecom and navigation satellites, as well as exploration spacecraft. The PPS®5000 was fully qualified in 2021.

The PPS®X00 plasma thruster (Hall effect) takes benefit of Safran’s long experience with electric propulsion to propose a very efficient product. PPS®X00 was designed to address the specific requirements inherent in the “New Space” market environment. With a lifespan exceeding 5,000 hours and very high specific impulse, the PPS®X00 is an extremely versatile thruster, making it ideal for all types of applications in its core market: low Earth orbit (LEO).

The SafeLaunch-FTR is based on more than 20 years of skills and experience. Such Flight Termination Receivers equip air to air, ground to air and air to ground missiles as well as UAV, target drones and Launch Vehicles. They are qualified under MIL-STD-810F and MIL-STD-461E standards, and comply to RCC-319. The compact and optimized package is consistent in size and weight with the most severe requirements of missile platforms. The electronical design, based on the latest generation of Software Defined Radio (SDR) components, brings to SafeLaunch-FTR high reliabilty and evolutivity.

Safran’s SEEING™ 130 Wide includes a unique medium focal length catadioptric optics, limited by diffraction only and with ultra-low distortion, offering perfect imaging over 35 mm full-frame image format. It is fitted with a 10megapixel sensor.  SEEING™ 130 Wide enables high Signal to Noise Ratio for multispectral (MS), hyperspectral (HS) and low light level imaging. SEEING™ 130 Wide includes a spectral filter with 23 bands covering Blue, Green, Red, Near InfraRed and Red Edge MS, for a broad spectral range between 475 and 900nm. SEEING™ 130 Wide has a large Field of View of 6.3° x 4.3° / 54 x 36 km2 from a 500km/310 miles orbit. In addition to its a thermal design within a robust structure, SEEING™ 130 Wide has a low SWaP, saving launch and operational costs.

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.