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September 18, 2025 Newsletter - SatNow

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Weekly Edition
Date: September 18, 2025
 
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Featured Space and Satellite Products
Space Qualified RF Filter
8.4-12.5 GHz Passive GaAs MMIC Bandpass Filter
Space Qualified RF Filter  from Marki Microwave

The MFBA-00004BH from Marki Microwave is a Passive MMIC Bandpass Filter with a passband from 8.4 to 12.5 GHz. It has a center frequency of 10.19 GHz with an insertion loss of 2.29 dB and provides a rejection of better than -20 dB. This BPF provides a return loss of 23 dB and has a group delay of 578 ps. This MMIC filter is available in a connectorized housing that measures 30.1 x 9.5 mm.
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Star Tracker
10-100 Arcsecond Star Tracker for High-Volume Applications
Star Tracker  from Rocket Lab

The ST-16HV from Rocket Lab is a Star Tracker with an absolute accuracy of 10-100 arcsec with a maximum slew rate of 2 deg/sec. This star tracker has an angular rate of 2 Hz with zero initial acquisition time and has a 2592 x 1944 CMOS active-pixel sensor. It requires a DC supply of 9-34 V and has a power consumption of up to 1 W. It has a mass of 148 g and measures 62 x 56 x 38 mm.
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SATCOM Redundancy Switch
Redundancy Switch System for SATCOM Applications
SATCOM Redundancy Switch  from WORK Microwave

The RSCM Series from WORK Microwave is a SATCOM Redundancy Switch with a frequency range of DC-40 GHz. This redundancy switch system has an insertion loss of 0.2-0.8 dB and an isolation of 50-85 dB. It requires a switching power of 1 W and has a switching time of 100-400 ns. The redundancy switch has a mass of 4 kg and measures 483 x 44 x 270 mm.
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Space Qualified RF Diplexer
Surface Mount Diplexer for GPS Applications
Space Qualified RF Diplexer  from Mini Circuits

The LDP-1050-252+ from Mini Circuits is a Space Qualified Diplexer designed to operate over a combined frequency range of 1-2500 MHz with defined passbands from 1–1050 MHz (low pass) and 1650–2500 MHz (high pass). It features a low insertion loss of 0.6-2.9 dB and a return loss of 6-17 dB. This RoHS-compliant diplexer has a mass of 0.02 g and measures 3.2 x 1.8 x 0.86 mm.
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Reaction Wheel
High-Precision Reaction Wheel for Imaging Satellites
Reaction Wheel  from Dragonfly Aerospace

The RW-1Nms from Dragonfly Aerospace is a Reaction Wheel that is designed for imaging satellites that demand exceptional platform stability and precise control while minimising disturbance torques. This reaction wheel has an angular momentum of 1.0 Nms and a torque of ±39 mNm. It has a rotation speed range of ±10000 rpm and supports CAN and RS-485 interfaces.
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Satellite Battery
23.1 V Lithium-Ferrite Modular Battery System for Small Satellites
Satellite Battery  from Berlin Space Technologies

The BAT-110 from Berlin Space Technologies is a Satellite Battery with a nominal voltage of 23.1 V and a capacity of 172 Wh. This flight-proven battery has a design life of 5 years in LEO. It is protected for over overcharging (non-destructive), tolerant against deep discharge (non-destructive), and offers cell balancing. It has a mass of 3 kg and measures 240 x 119 x 87 mm³.
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PCB Directory Launches their Inaugural Magazine for the PCB Industry
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
Space Qualified Solid State Relay
26.5 V DPDT Full Size General Purpose Signal Relay
Space Qualified Solid State Relay  from TE Connectivity

The 7-1617529-1 from TE Connectivity is a Space Qualified General Purpose Signal Relay with double-pole relay supports switching currents of up to 5 A at 28 VDC. The relay operates with a coil voltage range of 6.3-110 VDC and has a maximum coil power of 1.5 W. It offers a typical operating time of 5 ms and a release time of 5 ms. The insulation resistance is rated at 10,000 MΩ (minimum) at 500 VDC.
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Satellite Camera
4 MP Monochrome Camera for Space Domain Awareness Applications
Satellite Camera  from Infinity Avionics

The Lynx4MP-550 from Infinity Avionics is a 550mm ruggedized optical assembly with TRL 9 camera technology and can support precise image capture timing requirements. It has a spectral range of 400-1000 nm and a focal length of 550 mm. The RGB/Monochrome camera has a pixel resolution of 2048 x 2048. The camera has a mass of 1.5 Kg and measures 100 x 100 x 250 mm.
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Software Defined Radio
Integrated High-Speed Downlink Transmitter for SmallSat LEO missions
Software Defined Radio  from Honeywell Aerospace

The CDL-MS02 from Honeywell Aerospace is an Integrated High-Speed Downlink Transmitter that has a Tx frequency of 5100-5300 MHz and provides up to a 40 Mbps downlink to ground infrastructure. It requires a voltage supply of 28 V and has a variable output power of up to 5 W. This C-band transmitter weighs 1500 g and measures 179 x 232 x 47 mm.
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Satellite Terminal
1.8 m Ku-Band Auto Fly-Away Satellite Terminal
Satellite Terminal  from Norsat

The WFA180KU-NA from Norsat is a Satellite Terminal with an Rx frequency range of 10.7-12.75 GHz and a Tx frequency range of 13.75-14.5 GHz. This Ku-band antenna has an Rx gain of 45.3 dBi and a Tx gain of 46.3 dBi. It has an azimuth range of +/- 180 degrees and an elevation range of 0 to 90 degrees. It has a mass of up to 50 kg and measures 121 x 44 x 68 cm.
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Inertial Measurement Unit
Inertial Measurement Unit For Navigation Systems
Inertial Measurement Unit  from Seiko Epson Corporation

The M-G370PDT0 from Seiko Epson Corporation is a compact and lightweight Inertial Measurement Unit (IMU) that has low noise and high-accuracy measurements. It has an angular rate output range of ±200 °/s and features a bias instability as low as 0.8 °/h. It has an angular random walk of 0.03 °/√h and a velocity random walk of 0.02 m/s/√h. This IMU weighs up to 10 g and measures 24 × 24 × 10 mm.
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Satellite Solar Cell
High Efficiency Radiation Hardened Space Solar Cell
Satellite Solar Cell  from Rocket Lab

The IMM-a from Rocket Lab is a Satellite Solar Cell with a BOL efficiency of 32% at maximum power point and has a solar cell mass of 49mg/cm2. This solar cell has an open circuit voltage of 4.78 V and a current density of 10.12 mA/cm2 at maximum power. It has a voltage of 4.28 V at maximum power and a short-circuit current density of 10.66 mA/cm2.
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Satellite Modem
Software-Defined Satellite Modem for Communication Systems
Satellite Modem  from Digisat International

The QFlex-400 from Digisat International is a Satellite Modem with dual IF/L-band support that has a maximum data rate of 345 Mbps and an L-band frequency of 950-2450 MHz. This software-defined modem is fully qualified to DVB-CID standards and is suitable for applications such as IP trunking, cellular backhaul, fiber backup restoral services, corporate, and government services.
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Satellite Antenna
Ku-band Satellite Antenna for Geostationary Satellites
Satellite Antenna  from CTech

The SemaLink Hemispherical Antenna from CTech is a Satellite Antenna that has an antenna gain of more than -2.5 dBi and a VSWR of 1.119:1. The antenna is designed for geostationary satellites and is responsible for receiving RF signals sent from the ground or transmitting RF signals generated on board using the transmitters to the ground.
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Star Tracker
3-30 arcseconds Star Tracker for Nano-Satellites
Star Tracker  from TY-Space Technology Ltd

The NST4S-A2 from TY-Space Technology Ltd is a Star Tracker with an attitude accuracy of 3-30 arcsecs with a maximum slew rate of 3 deg/sec. This star tracker has an update rate of 10 Hz and an acquisition rate of 2 seconds. It requires a DC supply of 5 V and has a field of view of 15 x 18 degrees. It has a mass of 370 g and measures 57 x 57 x 182 mm.
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Antenna Positioning Mechanism
Antenna Positioning Mechanism for Motion Control Capabilities
Antenna Positioning Mechanism  from Kinematics

The KDE14 from Kinematics is an Antenna Positioning Mechanism with a backward holding torque of 54.4 kNm. It has an overturning moment of 47.4 kNm and is powered by hourglass worm technology for reliable accuracy. It is designed to allow for azimuth and elevation actuation in one complete assembly. It has 360-degree dual-axis torque with a raceway diameter of 345.5 mm.
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Satellite Link Emulator
600 MHz Propagation Channel Emulator for Satellite System
Satellite Link Emulator  from ECA Group

The PCE-600 from ECA Group is a Satellite Link Emulator with a bandwidth value of 600 MHz. The IMUX and OMUX filters of the system are based on complex FIR filters, and the non-linearity of the amplifier is improved with interpolation up to 1.8 GHz of instant bandwidth to avoid aliasing. It requires a supply voltage of 230 V and has a power consumption of 600 VA
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Satellite Electrical Power System
Modular Electrical Power System For CubeSats
Satellite Electrical Power System  from 2NDSpace SRL

The SOLO-EPS 4 from 2NDSPACE is a Modular CubeSat Electrical Power System (EPS) designed to provide robust and reliable power management for small satellite missions. It is configured with a Power Distribution and Control Unit (PDCU) and four Battery Management Systems (BMS) supporting CubeSats ranging from 1U to 27U. It has a mass of 480g and measures 97 x 92 x 44 mm.
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