The LEGION 400 tackles the new challenges of the space industry, offering enhanced connectivity, faster delivery, improved value, and unrivaled flexibility. 

This antenna system is designed to meet the demands of Earth Observation satellite tracking and the high-volume needs of Communication Satellite Constellations. 

What sets the LEGION 400 apart is its patented tri-band S/X/Ka concentric feed paired with a sleek and ultra-precise pedestal. It’s equipped to support LEOP & Launch Vehicles with its cutting-edge S-band Single Channel Monopulse auto track feed.

The ES9910 Ethernet switch/router, an advanced solution that offers seamlessly integrated, highly flexible, and fully managed LAN/VLAN connectivity for mission-critical systems.

This versatile technology serves onboard operations for both manned and unmanned ground, air, and sea vehicles, empowering them with top-notch networking capabilities.

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

These units undergo rigorous validation and formal qualification testing, adhering to standard test methods such as DO-160 and MIL-STD-810 to ensure their reliability and performance.

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.

• Typical accuracies of ±0.20°C 
• 16-channel isolated universal thermocouple/voltage inputs 
• Power over Ethernet+ (PoE+) 
• 20K samples/second/channel sample rate 
• 24-bit ADC per channel 
• 500 V channel-ground isolation 
• 1000 V channel-channel isolation 
• Data logger acquisition mode 
• Built-in parallel data streaming 
• Full-featured embedded web interface 
• LXI Ethernet interface 
• 8-bit bank isolated digital I/O 
• Compact 1U half-rack form factor

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.

Southwest Microwave’s high performance End Launch connectors are designed to provide low VSWR, mode free wideband response to 110 GHz for single-layer and multi-layer printed circuit boards where the high frequency signal is on the top layer. Available in SMA (27 GHz), 2.92 mm (K) (40 GHz), 2.40 mm (50 GHz), 1.85 mm (V) (67 GHz) and 1.0 mm (W) (110 GHz). 

Male and female options along with narrow body and bulkhead feed-through. Unique clamping mechanism accommodates board thickness up to .300” (7.62 mm). Robust, reusable and repairable. Multiple launch configurations provide the best possible match to circuit layout. Works on microstrip and grounded coplanar waveguide (GCPW) designs. Signal-layer microstrip and GCPW test boards available. Soldering is optional. 

Design Assistance: 

• Printed circuit board layout and connector part number recommendation 
• 3D models for mechanical layout 
• HFSS models (version 18.0 or newer) for EM simulations upon request and availability

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.

For microstrip or grounded coplanar waveguide (GCPW) designs, Southwest Microwave solderless vertical launch connectors provide optimal signal integrity and are reusable. Suitable for various board materials and thicknesses, the vertical launch connectors reduce footprint requirements without sacrificing performance, resulting in design and installation convenience.