Our patented miniaturized L/S/C Tri-Band Feed delivers top-notch performance and unmatched flexibility.

Equipped with a common L/S/C radiating front end, it’s complemented by a modular set of active RF modules, enabling simultaneous reception and tracking across various frequency bands. Its compact, lightweight design allows it to be mounted on any dishes ranging from 6 to 24 feet.

Available in single, dual, or tri-band configurations, this feed offers the best value for customers looking to meet current requirements while staying future-ready.

It’s also field-upgradable to add any missing bands with straightforward RF module additions, ensuring scalability while keeping costs in check.

• Spin mode is a dynamic mode intended to provide a simulation of a spinning satellite. 
• Enhanced Eclipse mode is a dynamic mode that allows the user to easily program and initiate an eclipse event with total control over all of the V-I curve parameters and dwell times. 
• Operates with Sequential Shunt Regulators and Maximum Power Point Trackers 
• Multiple redundant OVP/OIP layers

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.

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.

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®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).

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 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.