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 Mobile Telemetry Rack (MTR) integrates state-of-the-art telemetry capabilities utilizing the RTR-X4 & GMDR recorder providing the ideal portable telemetry checkout system, able to receive demodulation, record, process and display your data throughout your system development.

Based on the Cortex architecture, the 4U chassis-based CORTEX RTR-X4 can support up to four channels providing the utmost flexibility and capability a Telemetry Receiver can achieve.

The GMDR Chapter 7 recorder fits particularly well for the flight test support where operability and flexibility is essential. Not only the does the Telemetry rack provide a rich set of features, the Dell Server comes with the standard Safran software tools you expect: D4 Recorder, C10 Extract, eZ Viewer Data Verification and Quick Look Software.

Additionally, multiple projects can be supported by just swapping out the OS & media drives in support of classified projects.

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.

With its compact and rugged design, CMA is a perfect fit for data acquisitions in challenging environments and tight spaces.

CMA boasts the smallest size per channel, providing versatile acquisition modules to customize instrumentation for specific missile or New Space use cases. These acquisition modules enable software configuration in the field for each channel type.

Offering on-board processing, recording, hardware customization, GPS localization, and a built-in transmitter, CMA allows for an all-in-one-box solution.

CMA delivers advanced signal and acquisition conditioning, bus monitoring, recording, and transmission, all while reducing integration time, cost, and risk.

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 SafeLaunch-FTR is based on more than 20 years of skills and experience. Such Flight Termination Receivers equip air to air, ground to air and air to ground missiles as well as UAV, target drones and Launch Vehicles. They are qualified under MIL-STD-810F and MIL-STD-461E standards, and comply to RCC-319. The compact and optimized package is consistent in size and weight with the most severe requirements of missile platforms. The electronical design, based on the latest generation of Software Defined Radio (SDR) components, brings to SafeLaunch-FTR high reliabilty and evolutivity.

Configuring, managing, and integrating the system are crucial steps for ensuring the success of flight testing and achieving precise telemetry. eZ Software is your go-to solution. 

• eZ SetUp software allows to configure from a single acquisition unit to a complete acquisition system within a network architecture. 
• eZ Operation software is an advanced tool for centralized supervision and control of complex test systems from an onboard operator station. 
• eZ Processing / Advantys software offers advanced functions for data display and processing.

ARES (formerly IRIS) from Safran Defense & Space, Inc. (formerly Safran Data Systems, Inc.) represents the next-gen in transportable antenna systems. Packed in portable cases for easy handling, ARES can be shipped using standard methods and be fully operational in under an hour in the field, standing by to support satellites. Utilizing a reliable pedestal design and a dual-band concentric feed, ARES antenna ensures pinpoint accuracy and top-notch antenna performance. Crafted from standard (LRU) parts, it’s a breeze to maintain and service on-site, guaranteeing maximum uptime for all satellite missions. Combined with the SATCORE combo box (Command/Control modem & high-rate receiver) and the TM MAESTRO Monitoring & Control software, ARES is the all-in-one portable satellite tracking system.

The VS1410 is a video & data recorder/server packaged in a rugged compact chassis (3.75” x 5.75” x 7.36” / 6.4 lb), for recording on a Removable Memory Module (RMM).

Recorded data can be replayed in a standard PC/Windows® environment, using specific or COTS mission debrief solutions for post mission analysis. In addition, typically for ISR applications, data can be replayed while recording on board.

The ENERTEC™ mission data processing and distribution units offer cost-effective and dependable solutions for acquiring, processing, storing, exploiting, and disseminating field and mission data.

These units are suitable for both manned and unmanned ground, air, and sea vehicles. They undergo rigorous validation and formal qualification testing, adhering to standard test methods such as DO-160 and MIL-STD-810.