| | | | | | The integration connects two distinct air and missile defense architectures. Aegis is a shipboard, software-defined command-and-control system built around phased-array radar ... |
|
|
|
| |
|
|
|
| | Sponsored | | 6 channel VITA 62 OpenVPX. Wide temperature range at high power. Extended shock/vibration compliant. Onboard real-time clock. Switchable Battleshort and NED functions. Embedded RuSH™ technology monitors voltage, current, temperature and provides protective control. I2C interface Status & Control. USB port for status display, access menu control and firmware upgrade. Current sharing up to four modules. |
|
|
|
| |
|
|
|
| | | | The Air Force is looking for a persistent monitoring capability that can provide continuous, 24-hour surveillance of the RF spectrum to establish baseline activity, detect anomalies... |
|
|
|
| |
|
|
|
| | | | Built something that’s moving the needle in aerospace and defense? If it covers areas like C4ISR, trusted computing, electro-optics, embedded computing, RF and microwave, or software... |
|
|
|
| |
|
|
|
| | Sponsored | | LCRs RM Series are 19” rugged rackmount chassis for 3U VPX and SOSA aligned payloads. Ideal for use in demanding environments across a range of applications. The system supports 48.2 modules with 40Gb / 100Gb backplanes options. This chassis includes high CFM cooling fans. The 4U low profile chassis has a hinged front panel that enables easy payload access and provides EMI protection. |
|
|
|
| |
|
|
|
| | | | The agency is emphasizing approaches that leverage commercial spacecraft, launch, and mission operations, with a target for concepts that could be ready for launch by the third... |
|
|
|
| |
|
|
|
| | | | The contract supports integration of next-generation GPS IIIF spacecraft into the operational enterprise by ensuring the ground segment can execute launch, early orbit operations... |
|
|
|
| |
|
|
|
| | Sponsored | | The Ophir 150K-W Very High Power Laser Sensor measures power levels to 150kW. The water-cooled calorimetric sensor delivers exceptional accuracy and dependable performance over the range of 900-1100nm. Extremely low back reflection ensures operational safety. Designed for high-power directed energy systems, fiber laser development and testing, and industrial cutting and drilling. |
|
|
|
| |
|
|
|
| | Sponsored | | The future of military aviation is complex and ever-evolving. |
|
|
|
| |
|
|
|
| | | Harsh environments are challenging for electronic products. Design for Excellence (DFX) reviews help eliminate defect opportunities that could otherwise cause reliability issues. |
|
|
|
| |
| | | Technological Heritage & Safeguard Measures Our development process is rooted in a mature industrial chain and extensive flight heritage. We utilize a “design-for-success” methodology that integrates past mission data with rigorous safeguard measures. Learn More |
|
|
|
| |
|
|
|
| | | When failure isn’t an option, design for reliability. Discover how advanced packaging, thermal mitigation, parasitic control, and Silicon Carbide (SiC) integration deliver mission-ready high-power analog performance for aerospace and defense. |
|
|
|
| |
| | | Test engineers facing ATE obsolescence will gain practical guidance on spares, COTS, and FFF strategies including risk, TPS compatibility, software impact, and cost tradeoffs to extend legacy test system life. |
|
|
|
| |
|
|
|
| | | The material is specified with a dielectric constant (Dk) of 2.80 and dissipation factor (Df) of 0.0007, with stability across frequency up to 110 GHz and over temperature and moisture conditions. |
|
|
|
| |
| | | The Intellian OW7MP manpack terminal enables government and defense users to securely access Eutelsat’s global OneWeb LEO constellation in environments where traditional communications infrastructure is unavailable, degraded, or denied. |
|
|
|
| |
|
|
|
| | | The EDOF metalenses use a flat optical architecture to replace more complex multi-element assemblies, reducing system size, alignment requirements, and overall integration complexity. |
|
|
|
| |
| | | The BPE-35 is intended to address longstanding limitations of pressure-fed propulsion systems, which have traditionally been used with storable hypergolic propellants but impose mass and volume penalties due to pressurization hardware. |
|
|
|
| |
|
|
|
| | |
|
| | |
|