The CORTEX RSR-RF (-40 or -200) stands as a digital recorder that plays a vital role in capturing and reproducing the RF analog signal received by the antenna before any processing occurs.

It’s an essential component in a Telemetry Station, ensuring the utmost availability of crucial data, particularly in cases where on-board recording is not feasible.

Data collected in-flight offers extensive post-processing flexibility. You can fine-tune various settings in the receiver, the bit synchronizer, and the decommutator to maximize the extraction of data, a feat achievable only with RF recording. Furthermore, it serves as an invaluable tool for test range qualification ahead of test flights.

Our modular data acquisition unit, the XMA-ROTOR, brings cutting-edge module technology to the specialized mechanical housing designed for rotor head instrumentation. 

Say goodbye to outdated slip ring technology – the XMA-ROTOR revolutionizes the game by offering a completely wireless and contactless connection between the rotor and the stator. 

Power is transmitted through inductive coupling, while data, health monitoring info, configuration data, and synchronization signals are transferred over a bi-directional radio link.

The highly flexible modular GMDR system is a versatile and future-proof solution for acquisition, recording, dissemination and replay of FTI data in ground station applications. 

With its high integration, incomparable range of supported video interfaces and full compatibility with global leading MDR products, the GMDR integrates seamlessly into customers‘ existing test range topologies. 

With its intelligent data reduction through segmentation, pre-selection and filtering as well as the capability to freely disseminate subsets of data among several network destinations, GMDR efficiently reduces the operator‘s workload when analyzing test results. 

For standard PCM/Ch7-Telemetry applications, two simplified, cost-efficient variants with integrated PCM/Ch7-Telemetry signal boards and one Data Express technology (DE50)- compatible storage media slot are available.

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 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.

TM MAESTRO provides a comprehensive and centralized solution for monitoring and controlling telemetry infrastructure worldwide.

Designed to meet the critical needs of telemetry operators, this software offers a user-configurable GUI that adapts to various user profiles and mission phases, from preparation to live flight tests and station maintenance. TM MAESTRO is scalable and easily accommodates new telemetry equipment, allowing for the addition of an unlimited number of components, from antennas to decommutators, making it a highly flexible system.

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.

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.