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.

IRIS optical ground stations are built to cater to a wide range of applications (LEO/GEO/Probes), including Earth observation, high throughput bi-directional telecommunications, feeder link, or deep space missions. The IRIS systems leverage the Cortex Lasercom, a globally recognized optical modem that supports various standards such as SDA, CCSDS, and HPE.

Sensors acquisition and recording for troubleshooting is a cumbersome process in a fully furnished or operational aircraft, especially when time and low footprint are key drivers. 

This is no more the case with Safran new solution µMA: 

• its cylindrical form factor allows easy installation by just requiring a standard clamp used to mount tubes 
• its battery power supply and its wireless connectivity removes the need of installing any harness in the aircraft. 

All these capabilities are available while providing high measuring performance and harsh environment ruggedized in line with Safran standard solutions.

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).

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.

XONOS enabling high data volume downlink between satellite & ground station. It is our latest state-of-the-art qualified COTS based design perfectly adapted to NewSpace programs, where cost effectiveness, performances and reliability are success key factors.

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 RTR-X4 is one of the most advanced digital telemetry receivers on the market with its well-recognized RF performance and signal processing capability.

The 4U chassis-based RTR-X4 can support up to four channels providing flexibility and capability as well as a rich set of features for different frequency bands, modulations, decoders and output formats.

Not only does the CORTEX RTR provide an extensive set of features for different frequency bands, modulations, decoders and output formats, but the user can easily upgrade the equipment in the field to access additional and new features. The RTR-X4 is an excellent fit for flight test ranges, offering full flexibility and easy access to settings through its user-friendly GUI on the embedded 8.4-inch screen.