| Featured Space and Satellite Products |
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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 Transformer). It transforms a 50-ohm input into a 100-ohm Differential output and is tuned for optimal phase/amplitude balance. The balun has a maximum insertion loss of 6.5 dB and has an isolation value of 8 dB. It has a total input power value of 1 W and a VSWR value of 1.5. |
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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 single-ended GaAs frequency multiplier can amplify the input signal to an output power level of up to 13 dBm and has a fundamental rejection value of 20 dB. It requires a DC supply voltage of 6 V and has a current consumption of up to 250 mA. |
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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. The unit features low thermal sensitivity and magnetic sensitivity, ensuring consistent performance under extreme conditions. The atomic clock supports a bus voltage input of 26–48.5 V and has a power consumption value of 30 W in steady-state operation. It has a mass of 3.3 kg and measures 210 x 106 x 107 mm. |
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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. This launch vehicle platform uses carbon fiber composite material and has a Monocoque structure. It utilizes 1x Rutherford Vacuum propulsion engine in Stage 2 and 9x Rutherford Sea Level Engines in Stage 1. |
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| Dual Channel DVB-S2 X-Band Transmitter for LEO Spacecraft | |
Space Transmitter
from Dragonfly Aerospace
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| The HDRTx-3 from Dragonfly Aerospace is a dual-channel X-band transmitter tailored for micro and mini satellites in low Earth orbit. Featuring advanced DVB-S2 encoding, it maximizes data throughput, with each channel supporting symbol rates of up to 300 Msps for reliable, high-performance communication in space missions. |
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| 10.7-12.75 GHz Ku-Band Satellite Downconverter | |
Block Downconverter
from WORK Microwave
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| The VHBD-VSBD-VHBDR-VSBDR-Ku2Ku3 from WORK Microwave is a Block Downconverter that has an input RF frequency range of 10.7-12.75 GHz and an output frequency of 950-2000 MHz. This Ku-band downconverter has an LO frequency of 9.75-10.75 Hz and a phase noise of up to -140 dBc/Hz. The converter features automatic reference recognition and an adjustable gain equalizer. It weighs 6 Kg and measures 483 x 44 x 270 mm. |
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| SmallSat Mass Memory and Communications Protocol Unit | |
Satellite On-Board Computer (OBC)
from AAC Clyde Space
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| The SIRIUS TCM LEON3FT from AAC Clyde Space is a Satellite On-Board Computer (OBC) with a real-time operating system that runs on a 32-bit LEON3FT fault-tolerant processor. This command and data handling system consists of an onboard computer (Sirius OBC) and a combined mass memory with a CCSDS stack (Sirius TCM). It requires a power supply of 4.5-16 V. It has a mass of 130 g and measures 95.89 x 90.17 x 17.20 mm (L x W x H). |
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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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| L-Band Low Noise Amplifier for Space Applications | |
RF Amplifier
from ERZIA
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| The ERZ-LNA-0070-0300-20-0.7 from ERZIA is an RF Amplifier that operates in a frequency range of 0.7 to 3 GHz. This low noise amplifier has a small signal gain of 20-24 dB and an output power (P1dB) of 18 - 22 dBm. It has a gain flatness of ± 1.5 dB and a noise figure of 0.6 to 1 dB. The amplifier has a maximum input VSWR of 2.5:1 and an output VSWR of 1.5:1. It requires a DC supply voltage of 9-15 V and has a power consumption of 0.5 W. |
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| SmallSat Payload Power and Data Handling Unit | |
Payload Data Handling System
from Berlin Space Technologies
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| The PPDH110-1PL from Berlin Space Technologies is a Power and Data Handling Unit that is designed for small satellite payloads. It acts as the single interface unit between the bus and the payload. This power and data handling unit requires a DC input voltage of 20.5–25.2 V and supports RS-422 and LVDS payload data interfaces and RS-422 TMTC interface. It has an output voltage in the range of 3.8-23.1 V. It has a mass of 780 g and measures 186 x 98 x 46 mm. |
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| 2-18 GHz 5-bit Digital Attenuator for Satellite Communications | |
Space Qualified Variable Attenuator
from Qorvo
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| The CMD279C3 from Qorvo is a Space Qualified Variable Attenuator with a frequency range of 2-18 Hz. This attenuator has a low insertion loss of 3.5 dB and a return loss of 13 dB. It is controlled by a single voltage of either 0 V or +5 V to control RF signal levels over an attenuation range of 15.5 dB. It requires an input P1dB value of 27 dBm. The attenuator is Pb-free RoHS-compliant and is housed in a 3x3 mm QFN package. |
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| 4 Nms Reaction Wheels for Space Applications | |
Reaction Wheel
from Blue Canyon Technologies
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| The RW4 from Blue Canyon Technologies is a Reaction Wheel designed for very low Earth orbit to cislunar and interplanetary missions. It has a maximum torque of 0.25 Nm and a maximum angular momentum of 8 Nms. This reaction wheel has a high torque-to-speed ratio with a high-accuracy observer-based control design and supports RS-422 data interface. It requires a DC supply of 22-34 V and has a peak power value of 10 W. |
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| LizzieSat Platform for Microsatellite Constellations | |
Satellite Bus & Platform
from Sidus Space
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| The LizzieSat Platform from Sidus Space is a Satellite Bus & Platform with an orbital altitude of 300-650 km and has an orbital period of 90.4-97.6 minutes. It has a payload mass of 20-35 kg and has a payload volume range of 18-27 U. The platform has a payload data rate of 150 Mbps and has an RF output power range of 27-33 dBm.The platform has a bus voltage supply of 24-33.6 V. It has a total satellite mass value of 100 kg and measures 12 x 17.2 x 29 inches. |
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| Hold-Down & Release Actuator for Space Systems | |
Space Actuator
from ARQUIMEA
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| The REAC.153.V2.SX - 15KN - Nitinol from ARQUIMEA is a Hold-Down & Release Actuator (HDRA) designed for space applications requiring secure payload restraint and reliable release. This low-shock actuator supports a release load of 15 kN with an ultimate load rating of 22.5 kN. It has a proof load of 18.7 kN and has a shape memory alloy nitinol trigger system with redundant triggers for high reliability. The actuator accommodates misalignment at release up to ±2.5°. |
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| 3-axis Star Tracker for Small Satellite Applications | |
Star Tracker
from VECTRONIC Aerospace GmbH
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| The VST-41M from VECTRONIC Aerospace GmbH is a Star Tracker designed with a core element of the sensor’s processing electronics with a 512 x 512 pixel rad-hard CMOS sensor. It has an accuracy of 18-120 arcsec and an update rate of 4 Hz. This star tracker has a field of view of 14 x 14 degrees and an acquisition time of 800 ms. The star tracker requires a supply voltage of 9-40 V. It has a mass of up to 0.9 kg and measures 80 x 100 x 180 mm. |
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| 0.22-15 µH Space Grade Tin/Lead Shielded Inductor | |
Space Qualified Inductor
from Vishay
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| The IHLP-2020CZ-5L from Vishay is a Space-Qualified Inductor with an inductance range of 0.22-15 µH and an inductance tolerance of +/- 20 %. This tin/lead inductor has a direct current resistance of 3.95-195 mOhm and a self-resonant frequency of 14.1-190 MHz. It has a heat rating current of 2.4-18 A and a DC saturation current of 1.6-11 A. The inductor features a shielded construction with IHLP design and Tin/lead Sn/Pb-plated terminals. |
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| Satellite Link Emulator for Ground Station | |
Satellite Link Emulator
from dBm Corporation
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| The SLE9072 from dBm is a Satellite Link Emulator designed to provide a cost-effective, time-saving, and repeatable total solution for satellite-to-ground station RF link testing. This emulator has a maximum delay of 1400 ms per channel and has a VSWR of less than 1.5:1. It has a bandwidth of 72 MHz and has a center frequency of 70-140 MHz. The emulator has a doppler shift of 0-10 kHz. It has a mass of 32-35 lbs and measures 17 x 7 x 21 inches. |
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| 225-400 MHz SATCOM Fixed Helical Antenna | |
Earth Station Antenna
from TACO Antenna
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| The H-064A from TACO Antenna is a SATCOM Antenna that operates from 225-400 MHz frequency range. It has a gain of 11.9 dB and an axial ratio of 1.2 dB. This right-hand polarized antenna has a front/back ratio of 29.1 and a VSWR of 1:5:1. It has a maximum input power of 500 W and a cross-polarization rejection of 20 dB. This fixed helical antenna has a wind survival rating of 150 mph and has a wind area of 2.1 - 4.7 sq. ft and an impedance of 50 ohms. |
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| 10-Bit D/A Converter for Aerospace Applications | |
Analog to Digital Converter
from Analog Devices
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| The AD9731S from Analog Devices is an analog-to-digital converter that operates at a conversion rate of up to 170 MSPS. This D/A converter has a multiplying bandwidth of 75 MHz and an SFDR value of 66 dB. It has a resolution value of 10 bits and has an amplifier bandwidth value of 2.5 MHz. The requires an input voltage range of 0.8-2 V and has a power consumption of 439-449 mW. This converter measures 10.50 x 8.20 x 2 mm. |
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| 390L Propellant Tank for Satellites | |
Spacecraft & Satellite Propellant Tank
from Antrix Corporation Limited
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| The 390L Propellant Tank from Antrix Corporation Limited is a Spacecraft & Satellite Propellant Tank with a nominal internal volume of 390 L and a residual volume of 2.25 L. This propellant tank has an operating pressure of 16.5 bar and a burst pressure of 33 bar. It has a proof pressure of 24.75 bar with a maximum propellant flow rate of 80 cc/s. The propellant tank is constructed using Ti-6Al-4V commercially pure titanium and SS-304L. |
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| Satellite On-Board Computer (OBC) for Satellite Payload processing | |
Satellite On-Board Computer (OBC)
from SEAKR Engineering LLC
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| The RCC 5-CPB from SEAKR Engineering LLC is a Satellite On-Board Computer (OBC) that has an extended 6u CPCI module with PCI, GPIO, and SERDES interconnect. This OBC integrates three Virtex-5 FX-130T FPGAs with 3 GB DDR II SDRAM and 16 Gbits of configuration memory featuring onboard configuration storage with an optional scrubber. This conduction-cooled module is TRL9-rated and weighs 3.5 lbs. |
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