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.

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.

eZ Viewer is a data post-flight replay software for use with mission data based on IRIG-106 Chapter 10 format, recorded on ENERTEC recorder/server. This software is an easy-to-use, quick setup and intuitive tool targeted for data replay.

Key Features Comprehensive software tool for:

• Configuration of mission debriefing post-flight debriefing / mission analysis
• Data from on the media or archived

Intuitive interface:

• Pre-configuration of display
• Easy to use and quick setup
• SQUADRON mode

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 ENERTEC™ mission data processing and distribution units offer cost-effective and dependable solutions for field and mission data tasks, such as data acquisition, processing, storage, exploitation, and distribution. These units are suitable for use on both manned and unmanned ground, air, and sea vehicles. They undergo rigorous validation and formal qualification testing, adhering to standard test methods like DO-160 and MIL-STD-810.

The CORTEX RTR-X1 (formerly RX-1) is a compact, dual-channel telemetry receiver with a pre-D combiner, designed to span all IRIG frequency bands and conform to IRIG-specified modulations. 

This off-the-shelf (COTS) product leverages the rock-solid CORTEX RTR technology components, inheriting their renowned RF performance and signal processing prowess. 

The RX-1 excels in test range scenarios, offering cutting-edge features to ensure maximum data accessibility. Trust the RX-1 for top-tier telemetry reception in challenging conditions.

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.

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.

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.