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.

• SWIR (800-1800 nm) optimized
• 43.2 mm max. sensor size
• Focal length: 40 mm
• Initial aperture: F2.8
• Compatible to the V38-Mount System

• 2" (32 mm) max. Sensor size
• 3 focal lengths: 35 mm, 50 mm and 75 mm
• Very high resolution down to 2.4µm pixel size
• Initial aperture: F2.8
• M42 lens and TFL-Mount lens available
• Covering a wide working distance range

The RMM Manager utility software offers convenient, user-friendly pre-mission or post-mission access to SC1450-series Removable Memory Modules (RMM) for use with VS-Series video & data recorder/server, in PC/Windows® environment.

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).

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 D19-GT/-GTS Download Station ensures a secure and high-speed data download (via 40 Gbit Ethernet) from MDR or MDR-GT/-GTS storage media. Specifically designed for flight testing applications with demanding data rates and storage needs, the D19-GTS, when paired with MDR-GTS, incorporates advanced cybersecurity features like Data-At-Rest (DAR) protection and firmware updates. Configuration changes are facilitated through a Removable Secure Operational Disk (RSOD).

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, …

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.