| Featured Space and Satellite Products |
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| High-Power Differential Phase Shifter For RF Devices | |
Analog Phase Shifter
from Scientific Microwave Corporation
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| The WR187 from Scientific Microwave Corporation is a Analog Phase Shifter with a frequency range of 5.40-5.90 GHz. This phase shifter delivers exceptional performance with a typical VSWR of 1.20:1 across all port and has a low forward insertion loss of 0.2 dB. This 4-port water-cooled differential phase shifter integrates a hybrid coupler with H-bends and a ferrite-loaded phase shifter section to enable accurate differential phase control for dynamic beamforming and signal steering. It is ideal for high power industrial, scientific, radar systems and advanced communication platforms. |
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| OnBoard Computer for Global Satellite Applications | |
Satellite On-Board Computer (OBC)
from Airbus
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| The Amethyst from Airbus is a Satellite On-Board Computer (OBC) based on a high-performance ARM processor designed for safety-critical applications. This OBC has a 192 MBytes SDRAM CPU with error detection and 64 MBytes SDRAM IO with ECC. It interfaces with AOCS sensors and actuators, including magnetorquers and solar array step motors. This satellite on-board computer supports ethernet, SpaceWire, RS-422, and CAN bus interfaces. It measures 110 x 240 x 170 mm and is ideal for constellation applications and global satellite applications. |
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| 15 V Dual DC-DC Converter for High Reliability Applications | |
DC to DC Converter
from Crane Aerospace & Electronics
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| The MFL2815S from Crane Aerospace & Electronics is a DC to DC Converter with an input voltage of 28 V. This converter has an output voltage of 15 V and an output current of up to 4.33 A. It has an output power of up to 60 W and an output ripple of 30-110 mV p-p. The MFL converters are manufactured in a fully certified and qualified MIL-PRF-38534 facility and have an efficiency of up to 87%. The converter has a line regulation range of 0-20 mV and a load regulation of up to 20 mV. It is ideal for use in programs requiring high reliability, small size, and high efficiency. |
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| 10-20 MHz Space OCXO for GNSS modules Applications | |
Space Qualified Oscillator
from Rakon Limited
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| The ROD2522S2H from Rakon Limited is a Space Qualified Oscillator that synchronises its 1PPS and output clock to a specified 1PPS input signal from the GNSS system or the synchronization system output. It has a nominal frequency of 10-20 MHz and supports I²C bus interface for device status and command. This PPS Discplined oscillator has a frequency stability of 0.5 ppb and a phase noise of up to -155 dBc/Hz. The oscillator requires a supply voltage of 3.3 V. It is ideal for edge grand masters, DU/CU/servers, cell-site routers, front-haul switches, NIC time cards, test equipment and GNSS modules applications. |
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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 and functions in a 2+ kick stage. It uses carbon fiber composite material and has a Monocoque structure. 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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| Bipropellant Thruster for Attitude In-orbit Applications | |
Spacecraft Thruster
from AAC Clyde Space
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| The PM200 from AAC Clyde Space is a Bipropellant Thruster that has a thrust of 0.5 N and a specific impulse of 285 sec. This thruster can be used in 3-6U CubeSats and supports I2C, RS-422, and RS-485 interfaces. It features low system complexity and zero propellant toxicity that allows for simple and robust operations, both on the ground and when in orbit. This bipropellant thruster requires a supply voltage of 5-12 V and a power consumption of 0.1-12 W. It has a mass of 1.1 Kg and measures 97.7 x 95.4 x 95.4 mm. It is ideal for in-orbit maneuvers and Hohmann transfer orbit applications. |
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| Sponsored by PCB Directory | | PCB Directory Launches their Inaugural Magazine for the PCB Industry | | PCB Directory recently launched its Inaugural PCB Magazine for the PCB Industry. This magazine is packed with insightful articles, product listings, and an industry directory. The magazine is available in both print and digital versions. This achievement was made possible by the unwavering support of sponsors and contributors. Their trust and dedication have been the driving force behind this journey, and their support is highly appreciated. The team looks forward to continued growth and delivering even greater value to the PCB community. Click here to learn more. | | | |
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| 17.7-20.2 GHz Ka-Band SATCOM Low Noise Amplifiers | |
SATCOM Amplifier System
from Orbital Research
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| The WB Ka LNA from Orbital Research is a SATCOM Amplifier System with a frequency range of 17.7-20.2 GHz and a low noise temperature of 120 K. This Ka-band amplifier system has a gain of up to 55 dB and a gain flatness of ±1 dB over any 500 MHz. It has a gain stability of 0.2 dB and a ripple gain value of ±1.5 dB. The amplifier system has a P1dB value of 13 dB and has a maximum VSWR of 1.50:1. It requires a power supply of 10-28 V and has a maximum power consumption of 2 W. It is designed for satellite teleports and gateways, telemetry, tracking and command applications (TT&C) and airborne terminals. |
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| Space Qualified Multi-Mode Standard Transponder | |
Satellite Transponder
from General Dynamics Mission Systems
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| The MST-100 from General Dynamics Mission Systems is a Space-Qualified Multi-Mode Satellite Transponder with a transmitter operating frequency range of 2200-2300 MHz and a receiver operating frequency range of 1760-2120 MHz. This S-band transponder has a telemetry data rate of 1– 512kbps and a command data rate of upto 4 Kbps. It has a frequency stability of less than 0.5 ppm and a noise figure of 2.5 dB. It has a mass of 6 lbs. It is ideal to provide reliable earth-to-space craft, spacecraft-to-spacecraft communications, telemetry and command, proximity link and crosslink applications. |
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| 30000 Ohms GSFC Space Qualified Thermistor | |
Space Qualified Temperature Sensor
from TE Connectivity
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| The 44910 from TE Connectivity is a Space-Qualified Temperature Sensor with a resistance of 30000 ohms and a tolerance of ± 0.1 Deg C. It has a beta value of 3943 K and a beta tolerance of 0.4 %. It consists of a pressed disk ceramic sensor and thermally conductive epoxy coating that meet outgassing requirements. This GSFC S311-P18-01S7R6 qualified thermistor is ideal for extended space applications, low and mid-range temperature applications, tight tolerance instrumentation and applications requiring sensing small changes in temperature and outgassing. |
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| 1 m Ka-band Scorpion Manpack Satellite Terminal | |
Satellite Terminal
from Milexia Group
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| The Ka Band 1 m from Milexia Group is a lightweight and fully featured IP satellite terminal designed for secure and mobile communications. It operates in Ka-band that supports transmit frequencies of 29.0–31.0 GHz and receive frequencies ranging from 19.2–21.2 GHz. This 2-port circular polarized terminal is equipped with a 12 W BUC and maintains a transmitter VSWR of less than 1.25:1 and receiver VSWR of less than 1.5:1. This terminal has a terminal weight up to 20 kg and is ideal for defense, government and commercial users for reliable satellite communications in remote or challenging conditions. |
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| Mechanical Ground Support Equipment for Spacecraft | |
Assembly JIG
from Beyond Gravity
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| The MPT-G from Beyond Gravity is a Assembly JIG designed to support spacecraft and dedicated modules during horizontal and vertical integration. It enables electrically driven tilting from 0°–90° with extension up to 96°. It has an empty mass of 8730 kg and measures 6255 × 2945 × 1544 mm in horizontal position and 6255 × 2945 × 4260 mm in vertical position. The system is equipped for versatile handling through jacks, castors, towbar interfaces, forklift interfaces, facility cranes or optional air pads. It offers proven heritage for spacecraft integration and testing activities. |
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| High-Voltage Optocoupler For Space Applications | |
Space Qualified Optocoupler
from Southwest Research Institute
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| The 100SW1502 from Southwest Research Institute is a space-grade high-voltage optocoupler that has a forward voltage of 2.6-5.4 V at 200 mA. It features a 15 kV internal HV diode and provides up to 15 kV isolation between high-voltage and low-voltage sections. The device achieves a current transfer ratio (CTR) of 0.5-1.0% at 500 V depending on the LED configuration.It supports a very high stepping slew rate demonstrated by switching from 0 V to 10 kV on a 100 MΩ and has a load capacitance value of 40 pF. This radiation-tolerant optocoupler is ideal for high-reliability space applications. |
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| Multi-Constellation GNSS Receiver for Positioning in Space | |
GNSS Receiver
from NovaTel
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| The OEMStar from NovaTel is a GNSS Receiver with a horizontal position accuracy range of 0.5-1.5 m and a maximum data rate of up to 10 Hz. This receiver has a velocity accuracy of less than 0.05 m/s RMS and a time accuracy of up to 40 ns RMS. It has a time to first fix of less than 65 sec cold start and less than 35 sec hot start. The receiver requires an input DC voltage of 3.3-5 V and a power consumption range of 0.36 W. It provides precise positioning for space constrained applications and capable of tracking all current and upcoming GNSS constellations including GPS and GLONASS. |
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| Multi Constellation GNSS Simulator with Screen | |
GNSS Simulator
from Rohde & Schwarz
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| The SMBV100B from Rohde & Schwarz is a Vector Signal Generator with a frequency range from 8 kHz to 6 GHz. It delivers ultra-high output power of up to +34 dBm. It provides very low single-sideband phase noise of less than –134 dBc at 1 GHz and 20 kHz offset. The GNSS simulator is equipped with a 7-inch touchscreen interface for convenient operation and offers multiple connectivity options, including USB, LAN and GPIB. It is ideal for RF and envelope signal out of one box, real-time digital predistortion, GNSS testing, positioning accuracy testing, RAIM testing and ionospheric monitoring. |
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| 36V Radiation Hardened Dual Precision Operational Amplifier | |
RF Amplifier
from Renesas
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| The ISL70227SRH from Renesas is an RF Dual-Operation Amplifier for applications requiring both high DC accuracy and AC performance. This amplifier has a low input voltage offset of 10 µV and an input bias current of 1 nA. It features very low noise, low offset voltage, low input bias current and low temperature drift. This amplifier offers precision and a small footprint ensuring excellent value and flexibility. It is available in a hermetic ceramic flatpack and is ideal for applications such as precision and analytical instrumentation, active filters, precision power supply controls and industrial controls. |
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| High-Resilience Software Defined Radio for Communication Applications | |
Software Defined Radio
from Tethers Unlimited
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| The RAVEN-SDR from Tethers Unlimited is a Software Defined Radio that has a center frequency range of 75 MHz to 6 GHz. It has a large signal bandwidth of 200-500 MHz and a data throughput of 1-2 Gbps per channel. The system has an input power of +5 dBm and an input power value of -10 dBm. It features a wide array of electrical interfaces and AES encryption that provides high resiliency (Uptime) combined with high bandwidth on an adaptive platform. The SDR system requires an input voltage range of 22-34.6 V and has operating power of 23 W. It has a mass of 1 kg and measures 205 x 116 x 47 mm. |
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| L-band Rack Mounted Block Downconverter | |
Block Downconverter
from GeoSync Microwave
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| The GS5 Series from GeoSync Microwave is a Block Downconverter that has an input frequency range of 3.4-12.75 GHz and an output frequency range of 0.95-2 GHz. The block downconverter has gain value of 35 dB and a P1dB value of 18 dBm. The downconverter has a maximum noise figure value of 15 dB at minimum attenuation. It requires an input supply of 90-250 V AC and has a power consumption of 40 W. The converter has a maximum weight of 5.9 kg and measures 319 x 1.75 x 20 inches. It is designed for applications where frequency translation is needed between L-band and the transponder frequency. |
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| X-Band Low Noise Block for SATCOM Applications | |
Low Noise Block
from Communications & Power Industries
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| The TLNB-7500AS.0003 from Communications & Power Industries is an X-Band Low Noise Block Converter specially designed for SATCOM applications. It has an input frequency of 7.25-7.75 GHz and an output frequency of 950 to 1450 MHz. This LNB has an LO frequency of 6.30 GHz. This X-band LNB has an output power of +18 dBm and a VSWR of up to 1.25:1 (input) and 1.80:1 (output). This LNB utilizes state-of-the-art HEMT and GaAs FET technology enabling high reliability and stability. It measures 212.6 x 85.8 x 47.6 mm and is designed for both fixed and transportable applications. |
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| Space Qualified Solar Array Systems | |
Satellite Solar Panel
from SpaceTech GmbH
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| The Solar Arrays from SpaceTech GmbH are space qualified solar array systems designed to deliver up to 5 kW EOL power. These arrays provide a power-to-area density of 280–320 W/m² with a stiffness that exceeds 1 Hz for multi-hinge systems ensuring structural stability. It has a proven reliability of greater and have stowed stiffness of over 50 Hz out-of-plane and 120 Hz in-plane. The solar array have proven flight heritage in OneWeb Satellites, York Space Systems and a multitude of institutional missions, including GökTürk-2, Sentinel- 5p, Sentinel-6, EUCLID, FLEX, CHIME, CO2M, CRISTAL and LSTM. |
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| Hold-Down & Release Actuator for Space Systems | |
Space Actuator
from ARQUIMEA
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| The REAC.053.V2.SX - 5KN - Nitinol from ARQUIMEA is a Resettable Hold-Down & Release Actuator (HDRA) designed for space applications requiring secure payload restraint and reliable release. This actuator supports a release load of 5 kN. It has a proof load of 6.5 kN and has a shape memory alloy nitinol trigger system with redundant triggers for high reliability. It is ideal for applications include solar arrays, antennas, booms and masts, reflectors, cover doors, scientific instruments, shutter mechanisms, large structures, launch locks for gimbals, thrusters, stage separation and caging mechanisms. |
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| 3U Satellite Bus & Platform for Nanosatellite Missions | |
Satellite Bus & Platform
from ISISPACE
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| The CubeSat 3U Platform from ISISPACE is a Satellite Bus & Platform for nanosatellite missions. It has a payload volume of 1.5 to 2 U with a mass of up to 2kg/U and a data storage capacity of up to 64 GB. It supports I2C, SPI, UART and CAN interfaces for command and data handling. It supports average payload power up to 2W via 3V3 / 5V / 8V lines (2A max per line). This 3U platform has a TT&C uplink of up to 9.6 kbps and a payload data downlink of up to 3.4 Mbps. It is ideal for a wide range of applications, including satellite-based AIS, Earth Observation, astronomy and microgravity research missions. |
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| Ground Isolated Space-Qualified Accelerometer | |
Space Qualified Accelerometer
from Dytran Instruments
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| The 3133B3 from Dytran Instruments is a Ground Isolated Space-Qualified Accelerometer with a sensitivity of 5-10 mV/g. It has a frequency range of 0.25 to 10000 Hz and a resonance frequency of more than 35 kHz. It has a transverse sensitivity of 6% and an acceleration range of 1000 Gpeak. This accelerometer requires a compliance voltage of 18-30 VDC and a current range of 2-20 mA. It is available in a 4-pin Titanium housing that measures 7.6 x 6.6 mm with an integral cable of length 914 mm. This ground-isolated ultra-miniature accelerometer is ideal for low-frequency response. |
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| 40 mW Space Qualified Cryocooler for Space Missions | |
Space Cryocooler
from Sumitomo Heavy Industries
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| The 4He Cryocooler from Sumitomo Heavy Industries is a space-qualified cryocooler that provides a cooling capacity of 40 mW at 4.5 K. It has a power consumption of up to 50 W for the JT stage and up to 90 W for the Stirling stage. The 4K cryocooler has been successfully demonstrated in orbit, notably on the X-ray astronomical satellite Hitomi (ASTRO-H) and SMILES in ISS. The cryocooler has future deployment planned in missions such as XRISM and LiteBIRD and currently under development for advanced missions such as Athena and SPICA. |
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| Power Control and Distribution Units for Small Satellites | |
Power Conditioning and Distribution Unit (PCDU)
from Berlin Space Technologies
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| The PCU-110 from Berlin Space Technologies is a Power Conditioning and Distribution Unit (PCDU) with a design life of 5 years in low-earth orbit. It supports RS-422 TMTC interface and Schmitt Trigger intelligent power management for battery protection. This flight-proven PCDU requires a DC solar panel power range of 20-25 V and a regulated power range of 3.3-24 V. It has a latch protection with adjustable switched and fuses. The PCDU measures 236 x 105 x 87 mm. It is able to handle power regulation, power switching, DC/DC conversion and safety features of a small satellite. |
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