1727595

The 1727595 from Phoenix Contact is a cutting-edge Terminal Blocks - Panel Mount designed for next-generation aerospace applications. Featuring space-grade materials, this terminal block ensures flawless signal transmission in extreme conditions from stratospheric altitudes to deep space environments.The Header, Male Pins system utilizes gold-plated molybdenum contacts that maintain stable resistance across -200 C to +300 C thermal cycles. This reliability is critical for satellite payload connections experiencing 16 sunrises per day in LEO orbits.Engineered with hermetic sealing, the PCB Pins - Right Angle option provides outgassing rates below 1 10^-6 Torr-L/sec/cm , meeting NASA-STD-6012 requirements for vacuum applications in space telescopes and Mars rovers.Available in 1.904" (48.36mm) configurations, these terminals enable optimized PCB layouts for miniaturized CubeSat systems. The ultra-slim 5mm variant reduces mass by 60% while maintaining MIL-STD-883 shock resistance for launch vehicle applications.Compatible with 0.039 ~ 0.118" (1.0 ~ 3.0mm) specifications from 0.5mm to 6mm, the mounts adapt to both lightweight honeycomb panels and reinforced bulkheads. The iso-static mounting prevents stress concentrations in zero-G environments.The 3 matrix supports redundant ring-bus architectures essential for fault-tolerant flight control systems. This topology ensures continuous operation even with multiple point failures in avionics networks.The 2 Piece, Snap Lock - Front Flange incorporates vibration-damping alloy springs that survive 100G mechanical shock pulses per MIL-STD-810. This performance exceeds requirements for rocket-mounted telemetry systems during max-Q phase.Precision 0.300" (7.62mm) spacing prevents corona discharge in thin-atmosphere conditions. The polyimide insulation maintains dielectric strength at 0.1 Torr pressures encountered in high-altitude UAV applications.Rated for 300 V operation, the terminals withstand 15kV electrostatic discharges common in Martian dust storms. This protection is vital for planetary exploration equipment power systems.The 41 A capacity utilizes superconducting YBCO contacts for cryogenic satellite buses. These maintain <1n contact resistance at 77K in deep space probe power distribution networks.The Green coding uses phosphorescent markers for tool-free identification during EVA repairs. The pigments remain visible through astronaut gloves while resisting atomic oxygen degradation in ISS environments.The 1 single-plane construction minimizes magnetic susceptibility for star tracker applications. This configuration reduces compass deviation to <0.1 in Earth observation satellites.