| Featured Space and Satellite Products |
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| 10.70–12.75 GHz Dual Broadwall Coupler | |
Space Qualified Coupler
from Scientific Microwave Corporation
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| The WR75 from SMC is a space-qualified half-height dual broadwall coupler that operates in the frequency range of 10.70–12.75 GHz. This Ku-band coupler offers a forward coupling of 25.0 ± 1.0 dB and a directivity greater than 16 dB. It features a low insertion loss of 0.20 dB and an input VSWR of 1.20:1 that ensures minimal signal degradation. It is ideal for power monitoring, signal sampling, amplifier feedback control, and communication system applications in satellite and aerospace systems. |
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| 800-1175 MHz Power Splitter for Cellular Applications | |
Space Qualified Power Divider
from Mini Circuits
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| The SCN-2-11 from Mini-Circuits is a Space Qualified Power Divider that operates from 800-1175 MHz. It has a maximum phase unbalance of up to 3 degrees and an amplitude unbalance of 0.1-0.3 degrees. This space-grade power divider features a temperature-stable LTCC technology and wrap-around terminations for excellent solderability. It has a mass of 0.02 g and requires an input power of up to 20 W. The RoHS compliant power divider is ideal for GSM, ISM and cellular applications. |
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| 500 kHz to 6 GHz Surface Mount Broadband Balun | |
Space Qualified RF Balun
from Marki Microwave
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| The BAL-0006SMG from Marki Microwave is a broadband surface mount balun that operates from 500 kHz to 6 GHz (Balanced to Unbalanced X'former). It transforms a 50-ohm input into a 100-ohm Differential output and are tuned for optimal phase/amplitude balance. The balun has a maximum insertion loss of 6.5 dB. It has a total input power value of 1 W and a VSWR value of 1.5. It can be used in analog to digital converters, balanced receivers, baseband digital modulation and signal integrity. |
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| Three Analogue Fine Sun Sensor Assembly | |
Sun Sensor
from Berlin Space Technologies
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| The FSSA-110 from Berlin Space Technologies is a Sun Sensor that operates at 5 V. It has a power consumption of 185 mW and an accuracy of 5 deg. It has an update rate of 10 Hz and a radiation tolerance of more than 20 kRad. It offers hemispherical coverage and supports RS422 and 5x analogue channels/sensors. It can be placed in remote locations of the satellite and reports the sun vector back to the OBC. This flight-proven fine sun sensor assembly measures 95 x 44 x 20 mm. |
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| 5000 Ohms GSFC Space Qualified Thermistor | |
Space Qualified Temperature Sensor
from TE Connectivity
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| The 44906 from TE Connectivity is a Space-Qualified Temperature Sensor with a resistance of 5000 ohms and an interchangeability of +/- 0.1 Degrees C. It has a beta value of 3891 K and a thermally conductive epoxy coating that exhibits less than 0.66% TML and 0.10% WVR. This GSFC S311-P18-01S7R6 qualified thermistor is ideal for extended space, low and mid-range temperature, tight tolerance instrumentation and applications requiring sensing small temperature changes. |
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| 25 GHz Frequency Doubler for Space Applications | |
Space Qualified Frequency Multiplier
from Teledyne e2v HiRel Electronics
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| The TDFM001000 from Teledyne e2v HiRel Electronics is a Space Qualified Frequency Multiplier that up-converts an input frequency from 7.5-25 GHz to an output frequency from 15-50 GHz. This doubler is fabricated using a GaAs PHEMT technology which is based on electron beam lithography to ensure high repeatability and uniformity. It is ideal for satellite transponders, transmit/receive modules, microwave-based communications, millimeter-wave point-to-point radio and related applications. |
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| Rubidium Atomic Frequency Standard for GNSS Applications | |
Space Qualified Atomic Clock
from Airbus
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| The RAFS from Airbus is a space-qualified atomic clock that delivers a 10.00 MHz output based on the Rb87 atomic spectral absorption line. It has a mass of 3.3 kg and measures 210 x 106 x 107 mm. It has a design life of over 15 years and is suited for LEO, MEO and GEO missions. This space-grade atomic clock has proven in missions like Giove-A/B, Galileo and ISRO programs. It is ideal for GNSS overlay systems, navigation payloads, high-performance communications and scientific instruments. |
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| Sponsored by Crane Aerospace & Electronics | | |
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| Software Defined Radio For Small Satellites | |
Software Defined Radio
from Blue Canyon Technologies
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| The SDR from Blue Canyon Technologies is a space-qualified software-defined radio that supports downlink frequencies of 2.2–2.5 GHz (S-band), 8–8.5 GHz (X-band), and 21–33 GHz (Ka-band) and has an uplink frequencies of 1.76–1.84 GHz (L-band), 2.0–2.11 GHz (S-band) and 21–33 GHz (Ka-band). This full-duplex SDR integrates high-efficiency modulation schemes including BPSK, OQPSK, QPSK, 8PSK, and 16APSK with CCSDS-TC (uplink), CCSDS-TM and DVB-S2 (downlink) protocol support. |
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| Electron Launch Vehicle Platform | |
Satellite Launch Vehicle Platform
from Rocket Lab
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| The Electron from Rocket Lab is a Satellite Launch Vehicle Platform designed specifically to place small satellites of up to 300 kg into a wide range of low earth orbits (LEO). It has a vehicle mass of 13,000 kg. This launch vehicle has a thrust of 5800 LBF in Stage 2 and 5600 LBF in Stage 1 which incorporates pneumatic unlocking and springs fairing separation system. It uses liquid oxygen and kerosene as propellants and has proven flight experience with NASA, DARPA and US Air Force. |
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| 10 Kohms Space-Qualified Gold Chip Temperature Sensor | |
Space Qualified Temperature Sensor
from Variohm Eurosensor
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| The 10K3CG1269 from Variohm Eurosensor is a Space-Qualified Temperature Sensor with a nominal resistance value of up to 10000 ohms and a tolerance of +/-5%. This HI-Rel sensor possesses excellent stability with MEAS ceramic and has a flight heritage of 20 years. This high-reliability gold chip space-qualified temperature sensor measures 0.889 x 0.889 x 0.305 mm and is ideal for satellite camera systems, satellite telecom systems, temperature compensation and control panel monitoring. |
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| Orbital Class Reusable Launch Vehicle Platform | |
Satellite Launch Vehicle Platform
from SpaceX
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| The Falcon 9 from SpaceX is a reusable two-stage Satellite Launch Vehicle Platform designed for reliable and safe transport of people and payloads into Earth orbit and beyond. It has a payload capacity of 22800 kg to LEO, 8300 kg to GTO and 4020 kg to Mars. This satellite launch vehicle platform uses liquid oxygen and kerosene as propellants and serves a range of low-Earth orbits including services to low-inclination orbits through high-inclination and sun-synchronous orbits (SSO). |
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| 45 V High-Efficient Schottky Rectifier for Space Applications | |
Space Qualified Diode
from Infineon Technologies
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| The 30CLJQ045 from Infineon Technologies is a Space Qualified Diode with a maximum DC reverse voltage of 45 V and a maximum average forward current of 30 A. It has a maximum junction capacitance of 375 pF. It features a guard ring for enhanced ruggedness and has a surface mount hermetically sealed package measuring 70 x 92 mm. It is fully qualified according to MIL-PRF-19500 for space applications and is suitable for high frequency switching power supplies and resonant power converters. |
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| 7.1-8.5 GHz X-Band Hybrid Coupler for Nanosatellites | |
Space Qualified Coupler
from WiRan
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| The CXA from WiRan is a Space Qualified Coupler with an operating frequency range of 7.1-8.5 GHz. The coupler has a return loss of greater than 17.5 dB and has a power handling capacity of less than 30 W. This X-band coupler has a mass of 35 g and allows for easy and reliable splitting of an input RF signal equally between two output ports with a 90-degree phase shift. It features low insertion loss, low VSWR, high power handling and high isolation. This coupler is ideal for nanosatellite applications. |
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| 1K x 36-bit Radiation Hardened First-In First-Out Memory | |
Space Qualified Memory
from Honeywell Aerospace
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| The HX6136 from Honeywell Aerospace is a Space Qualified Memory with a configuration of 1K x 36 memory. It has a write access time of 36 ns. The memory cell is single event upset hardened with multi-layer metal power busing and small collection volumes of SOI provide superior single event effect and dose rate hardening. This space-grade SRAM is designed for a wide variety of data buffering needs, including high-speed data acquisition, multiprocessor interfaces and communications buffering. |
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