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October 30, 2025 Newsletter - SatNow

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Weekly Edition
Date: October 30, 2025
 
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Featured Space and Satellite Products
Space Qualified RF Balun
500 kHz to 6 GHz Surface Mount Broadband Balun
Space Qualified RF Balun  from Marki Microwave

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 are 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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Space Qualified Frequency Multiplier
25 GHz Frequency Doubler for Space Applications
Space Qualified Frequency Multiplier  from Teledyne e2v HiRel Electronics

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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Software Defined Radio
Software Defined Radio For Small Satellites
Software Defined Radio  from Blue Canyon Technologies

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). It delivers a data rate of up to 100 Mbps and has an adjustable RF output power with a maximum value of +35 dBm.
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Satellite Launch Vehicle Platform
Electron Launch Vehicle Platform
Satellite Launch Vehicle Platform  from Rocket Lab

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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Space Qualified Circulator
1-2 GHz Three-Port Double-Ridged Coax Circulators
Space Qualified Circulator  from Scientific Microwave Corporation

The 1-2 GHz Circulator from Scientific Microwave Corporation is a 3-Port Circulator that operates from 1 to 2 GHz. It has an insertion loss of 0.6 dB and provides an isolation of 14 dB. This circulator can handle a peak input power of up to 20 kW. This double-ridged circulator has high-power handling for average and peak powers, combined with low loss and VSWR, making this circulator a very sought-after addition to any EMC system.
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Satellite Camera
12 MP RGB/ Monochrome Camera for Space Applications
Satellite Camera  from Infinity Avionics

The ORION12MP from Infinity Avionics is a 12 Megapixel RGB/ Monochrome Satellite Camera that provides high FPS image capture capability with on-board non-volatile data storage options. It has a pixel size of 5.5 um and has a pixel resolution of 4096 x 3072. The camera can capture and save images in non-volatile memory with an on-board storage of 256 GB, with up to 290 full-resolution images. The camera has a mass of 500 g and measures 100 x 100 x 55 mm.
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Sun Sensor Simulator
Light Stimulator for Sun Sensors OGSE for TVAC
Sun Sensor Simulator  from Solar MEMS

The LS3 from Solar MEMS is a Sun Sensor Simulator that is based on a controlled and stable light source to stimulate optical sensors. This optical ground support equipment has a beam size diameter of 25 mm and a focal length of 18 mm. It has a beam homogeneity of greater than 90 % and a light collimation of less than 10 degrees. The simulator has a light spectrum range of 450-1100 nm and supports Modbus RTU over RS-232 communication interface.
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Space Qualified Temperature Sensor
30000 Ohms GSFC Space Qualified Thermistor
Space Qualified Temperature Sensor  from TE Connectivity

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 (0°C to 70°C). It has a beta value of 3943 K and a beta tolerance of 0.4 %. This flight-proven temperature sensor has a dissipation constant of 1 mW/°C and an insulation resistance of 500 V. It consists of a pressed disk ceramic sensor and thermally conductive epoxy coating that meet outgassing requirements.
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Antenna Positioning Mechanism
25.5-27 GHz Hemispherical Antenna Pointing Mechanism
Antenna Positioning Mechanism  from Airbus

The LEO Ka-Band from Airbus is an antenna pointing mechanism designed for hemispheric coverage in low Earth orbit communications. It offers a pointing accuracy of less than 0.3° and a rotational velocity under 10°/s. It has a frequency range of 25.5–27 GHz and delivers a high antenna gain of 31 dBi. This has an independent 2-axis movement with full azimuth rotation and variable elevation. The unit has a mass of less than 9 kg and a moving envelope of 70 x 72 cm.
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GNSS Receiver
GNSS Receiver Module for Accurate Muzzle Velocity Testing
GNSS Receiver  from ReliaSat

The W-x8RX-RA-9296 from ReliaSat is a GNSS Receiver with an RF frequency range of 92-96 GHz and an IF frequency range of 2-6 GHz. This receiver has a LO frequency of 10.80–11.40 GHz and has an image rejection of 20 dB. The module contains Arralis monolithic millimetre-wave p-HEMT integrated circuits and patented technology allowing very large-scale integration. The receiver has a mass of 90 g and measures 28 x 57 x 24 mm.
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Satellite On-Board Computer (OBC)
Single Board Computer for Space Payload and Communication Processing
Satellite On-Board Computer (OBC)  from SEAKR Engineering LLC

The Athena-3 SBC from SEAKR Engineering LLC is a Satellite On-Board Computer (OBC) that has 2450 DMIPS, PowerPC e500 core, VxWorks RTOS, and Linux RTOS systems. It has a memory of 1 GB DDR II SDRAM and has an EEPROM memory of 128 Kbytes. This single board computer integrates two SpaceWire ports, three bi-directional RS-422 ports, one 1000 bT Ethernet port, and one dual/reductant 1553 port.
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RF Amplifier
5.725-6.725 GHz Redundant Line Amplifier System
RF Amplifier  from Narda-MITEQ

The RL3-572672 from Narda-MITEQ is a dual 1:1 Redundant Line Amplifier System designed to ensure uninterrupted signal transmission in satellite communication networks. It operates over a frequency range of 5.725-6.725 GHz and provides a minimum gain of 30 dB with options for higher gain configurations. It has an isolation greater than 50 dB. This amplifier system weighs up to 9.17 kg and measures 19 × 1.75 × 22 inches.
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Space Qualified Thermal Strap
Space-Qualified Thermal Strap for Cryogenics and Spacecraft
Space Qualified Thermal Strap  from Thermal Management Technologies

The TMT010-302 from Thermal Management Technologies is a Space Qualified Thermal Strap that facilitates the transfer of heat while retaining elastic connections between thermal components. It is a braided construction using copper with a braid width of 6.35 mm, length of 127.00 mm and an end height of 5.08 mm. The thermal strap has 1 hole of diameter 2.413 mm and has a resistance of up to 33.65 K/W at 295 K.
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SATCOM Antenna
Ku-band Phased Array SATCOM Antennas for Mobile Platforms
SATCOM Antenna  from BAE Systems

The Ku Band Multi-Orbit LEO Antenna from BAE Systems is a Ku-band phased array antenna that supports access to GEO, MEO and LEO networks. It can dynamically optimise communication link performance by switching between networks, ensuring connectivity across all constellations and scan angles. It has a Tx frequency of 13.75-14.50 GHz and an Rx frequency of 10.70-12.75 GHz. This ESA has a gain-to-noise temperature of 13.2 dB/K.
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Power Processing Unit for Thruster
Multi-Functional Propulsion Power Unit for Thrusters
Power Processing Unit for Thruster  from ASP-Equipment

The SPICA-virtus PPU for HET from ASP-Equipment is a multifunctional and multi-thruster Propulsion Power Unit (PPU) optimized for satellite constellation missions and related applications. It is designed to operate various HEMPT thrusters, including the HEMPT EV0, BUSEK BHT350, and BUSEK BHT600, simply through configuration without hardware modification. The PPU weighs 4.2-6.3 kg and measures 372 × 182 × 50 mm.
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Spacecraft Thruster
20 N Hydrazine Monopropellant Thruster for Satellites
Spacecraft Thruster  from IHI Aerospace

The MT-2 from IHI Aerospace is a Hydrazine Monopropellant Thruster that has a thrust value range of 6.9-19.6 N and has a specific impulse value range of 210-226 s. This monopropellant thruster has an operable pressure of 0.48-2.76 MPa and has 261914 number of pulses. It is a high-reliable thruster system that has a thruster mass of 115 kg and is designed for flight-proven applications.
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Satellite Bus & Platform
500 W Satellite Platform for LEO Missions
Satellite Bus & Platform  from SPUTNIX

The Pallada from SPUTNIX is a Satellite Bus & Platform with an average power supply system capacity of 500 W and a maximum power supply system of up to 1000 W. It has an onboard TM/TC system frequency range of 2000-2200 MHz and a data rate of up to 1 Mbps. The platform has an interface with ground payload data receiving complex with a frequency range of 8000-8100 MHz and a data rate of 800-1500 Mbps.
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Space Qualified Accelerometer
Triaxial Space-Qualified Accelerometer
Space Qualified Accelerometer  from Dytran Instruments

The 3133D1T from Dytran Instruments is a Triaxial Space-Qualified Accelerometer with a sensitivity of 0.25-10 mV/g. It has a frequency range of 0.3-6000 Hz and a resonance frequency of more than 35 kHz. It has a sensitivity tolerance of 20%. It is available in adhesive mounting and is ideal for use in Environmental Stress Screening (ESS), HALT/HASS, Modal and structural analysis, Product response testing, and General-purpose triaxial vibration measurements.
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Satellite Electrical Power System
Space Qualified Satellite Electrical Power System for CubeSats
Satellite Electrical Power System  from DHV Technology

The NanoEPS from DHV Technology is a Space Qualified Satellite Electrical Power System designed for 2U, 3U, 6U, and 12U CubeSats, providing efficient power generation, management, and storage for small satellite missions. It consists of a power management module and a battery module, ensuring reliable performance across various CubeSat configurations from non-deployable 3U or 6U platforms to triple deployable 2U/3U/6U and double deployable 12U systems.
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Space Transmitter
S-Band Transmitter SDR for Small Satellites
Space Transmitter  from IQ spacecom

The HiSPiCO from IQ spacecom is a Space Transmitter that operates at a transmit frequency range of 2.20-2.29 GHz and a transmit RF bandwidth of 1.3 MHz. It has a payload data rate of up to 1.6 Mbps and a linear RF output power value of 27 dBm. This TRL-9 rated space transmitter requires a supply voltage of 3.3-5 V and a low power consumption of 5 W. It has a mass of 100 g and measures 95 x 46 x 15 mm³.
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