| Featured Space and Satellite Products |
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| 600-1200 MHz Ceramic Balun for GSM Applications | |
Space Qualified RF Balun
from Mini Circuits
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| The TCN2-122+ from Mini Circuits is a Space Qualified RF Balun with a wideband frequency range of 400-1200 MHz. This ceramic balun has an amplitude unbalance of 0.3 dB and a low phase unbalance of 4 degrees. It has an impedance ratio of 2 and a maximum insertion loss of 1 dB. The balun has an impedance value of 50 Ohms and a maximum RF power rating of up to 3 W. This RoHS-compliant balun has a mass of 0.02 g and measures 0.12 x 0.06 x 0.037 inches. |
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| GNSS Receiver for LEO and GEO Orbits | |
GNSS Receiver
from General Dynamics Mission Systems
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| The Sentinel M-Code GPS Receiver from General Dynamics Mission Systems is a Space-Qualified GNSS Receiver that is designed for LEO, GEO, MEO, and HEO applications. It has a DC power consumption of about 9 W for LEO and 8 W for GEO orbits. This radiation-hardened receiver is immune to single-event latch-up and is suitable for velocities up to 16,000 m/s. This GNSS receiver has a mass of 2.5 Kg and measures 180 x 160 x 160 mm. |
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| 40 Wh CubeSat Battery for LEO Missions | |
Satellite Battery
from AAC Clyde Space
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| The OPTIMUS-40 from AAC Clyde Space is a Satellite Battery with a capacity of 40 Wh. This battery has a charge/discharge current of 2.6 A and a charge/discharge rate of 1.53 (fraction of capacity), discharge voltage limit. It has a minimum discharge voltage limit of 6.2 V and a maximum charge voltage limit of 8.4 V. The battery has a quiescent power consumption of less than 0.1 W. It has a mass of 335 g and measures 95.89 x 90.17 x 27.35 mm. |
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| Non-Pyrotechnic Space Vehicle Separation System | |
Separation System
from Rocket Lab
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| The 2003336B from Rocket Lab is a Separation System that is designed to separate space vehicles from launch vehicles. This mechanical separation system has a bolt circle diameter of 8-24 inches and can support payloads of up to 200 Kg. It is TRL 9 qualified and is made with materials and methods consistent with Class-A space flight hardware. The separation system has a total mass of 3000 Kg. It requires a supply voltage of 24-32 V. |
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| Three-Axis Magnetometer for CubeSat Missions | |
Magnetometer
from CubeSpace
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| The CubeMag GEN 2 from CubeSpace is a three-axis magnetometer built for robustness and including a backup sensor. The sensor comes in a compact or deployable version for satellites with larger magnetic disturbances. It has a noise per channel range of 50-120 nT. The magnetometer has an update rate of 5 Hz with a radiation value of 24 kRad. It has a mass of 16 g for the deployable module with a mass of 6 g for the compact module and measures 17 x 6.5 x 82 mm. |
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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. It requires an input power bus voltage of 22-38 V. It has a mass of 3.5 Kg and measures 110 x 240 x 170 mm. |
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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%. It measures 3.005 x 1.505 x 0.400 inches. |
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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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| Integrated High-Speed Downlink Transmitter for SmallSat LEO missions | |
Software Defined Radio
from Honeywell Aerospace
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| The CDL-MS02 from Honeywell Aerospace is an Integrated High-Speed Downlink Transmitter that has a Tx frequency of 5100 to 5300 MHz and provides up to a 40 Mbps downlink to ground infrastructure. It comprises a radio transmitter with a high-efficiency GaN SSPA, a power distribution unit providing accurate regulation and delivery of power across the system, and a digital baseband. This C-band transmitter weighs 1500 g and measures 179 x 232 x 47 mm. |
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| 3.4-4.2 GHz C-Band Low Noise Block with External Reference | |
Low Noise Block
from Orbital Research
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| The 3400X from Orbital Research is a Low Noise Block with an input RF frequency of 3.4-4.2 GHz and an IF frequency of 950-1750 MHz. This LNB provides a bandwidth of 500-800 MHz and has a noise figure of 0.25 dB. It has a gain of 60 dB and has a gain ripple value of ± 1 dB. This LNB has an image rejection value of 45 dBc and has a P1dB compression value of 10 dBm. It requires a DC supply of 12-24 V. It has a mass of 580 g and measures 144 x 68 x 39 mm. |
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| 1.8 m Ku-Band Auto Fly-Away Satellite Terminal | |
Satellite Terminal
from Norsat
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| 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 an interfacility link cable of 10 m and a reflector diameter of 1.8 m. It has a mass of up to 50 kg and measures 121 x 44 x 68 cm. |
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| Horizon Sensor for Nano Satellites | |
Earth/Horizon Sensor
from Solar MEMS
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| The HSNS from Solar MEMS is a Quad Thermopile Horizon Sensor that has an accuracy of less than 1° (EOL). It has an output data rate of 10 Hz and a field of view of ±2.5 degrees of reach IR eye. This sensor can measure infrared radiation from space and earth with 4 IR eyes with accuracy, and supports UART and I2C electrical interfaces. It requires a supply voltage of up to 5V. The sensor has a mass of 0.12 Kg and measures 90 x 92 x 50 mm. |
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| 64 Mb Magneto resistive Memory for Space Applications | |
Space Qualified Memory
from Honeywell Aerospace
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| The HXNV06400 from Honeywell Aerospace is a Space-Qualified Memory with a configuration of 8M x 8 or 4M x 16 memory. It is fabricated with Honeywell’s silicon-on-insulator CMOS technology that has a write access time of 150 ns and a storage capacity of 64 Mb. This memory has a read access time of 100 ns and delivers long-term data integrity for critical applications like processor code storage and fast access times for re-writeable data logs. |
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| 8-bit Monolithic Analog-to-Digital Converter | |
Analog to Digital Converter
from Analog Devices
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| The AD9283S from Analog Devices is an analog-to-digital converter that operates at a conversion rate of up to 100 MSPS. It is equipped with an on-chip track-and-hold circuit and is optimized for low cost and low power. This A/D converter has an analog bandwidth of 475 MHz and a signal-to-noise ratio (SNR) of 46.5 dB. It has an analog input range of 1 Vp-p and a low power of 90 mW. It is available in a CMOS-fabricated 20-lead package measuring 7.64 x 7.50 x 1.98 mm. |
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| DC to 26.5 GHz Space Qualified Flexible RF Cable Assemblies | |
Space Qualified Cable Assembly
from Amphenol CIT
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| The MCJ205A from Amphenol CIT is a Space Qualified Cable Assembly with a maximum frequency value of 26.5 GHz. It has a maximum insertion loss of 1.28 dB/m and has an impedance value of 50 ohms. The cable assembly has a power handling capability of 326 W and a low SWR of 1.25:1. It is constructed using a low or ultra-low density PTFE dielectric offering excellent loss characteristics, phase stability, flexibility, and light weight. |
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| Digital Phase Shifter For Satellite Communications | |
Space Qualified Digital Phase Shifter
from Scientific Microwave Corporation
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| The WR284 from Scientific Microwave Corporation is a Space Qualified Digital Phase Shifter designed for high-power microwave applications. It operates at a frequency of 2997.924 MHz with a maximum VSWR of 1.10:1. This phase shifter provides a full 0-360° phase range with a fine resolution of 1.4° across 256 digital steps. It supports peak power handling below 40 MW and average continuous power up to 1.5 kW CW. |
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| 58 L Propellant Tank for Spacecrafts | |
Spacecraft & Satellite Propellant Tank
from Orbital Propulsion Centre
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| The EPDM - BLADDER TANK BT 01/0 from Orbital Propulsion Centre is a Spacecraft & Satellite Propellant Tank with a net tank volume of 58 L and a maximum expected operating pressure of 26 bar. This propellant tank is compatible with hydrazine propellant and pressurant gases such as helium and nitrogen. It has a proof pressure of 39 bar and a burst pressure of 52 bar. The tank has a spherical geometrical shape and has a tank mass of 8.5 Kg. |
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| 2-Phase Bi-Axis Gimbal for Antenna Pointing Mechanism | |
Gimbal
from Sierra Nevada Corporation
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| The C14 from Sierra Nevada Corporation is a Bi-axis Gimbal with a 2-phase stepper motor designed for high stiffness, fine pointing accuracy, and long operational life. The gimbal has a step size of 0.0625° and a maximum output torque value of 14 Nm. It has a maximum axial load capacity of 6338 N and has a maximum radial load capacity of 1223 N. This gimbal has a winding inductance value of 30 mH and has a winding resistance of 57 ohms. |
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| Digital CubeSat Camera Module for Space Imaging | |
Satellite Camera
from SATLANTIS
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| The iSIM-90 from SATLANTIS is a high-resolution satellite imaging payload that delivers a ground sampling distance (GSD) of 2 m in PAN & VNIR and 5 m in SWIR at 500 km altitude. This ultra-high resolution optical payload provides a swath width of 13-23.5 km in PAN & VNIR and 8.2 km in SWIR, offering flexible coverage for diverse applications. It supports multispectral imaging across VNIR and SWIR bands. The optical imager system has a mass of less than 4 kg. |
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| 43.8 bar Low Pressure Stainless Steel Value | |
Spacecraft Valve
from Moog
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| The 050E880 from Moog is a Spacecraft Valve with a maximum operating pressure of 43.8 bar. It has a proof pressure of 66.2 bar and a burst pressure of 111 bar. This valve has a cycle life of 150 cycles and is opened/closed by rotating an actuation nut. The ground connection is a standard AN-style fitting that can be attached before operating the valve. This valve weighs 209 g and has a stainless steel/ titanium construction measuring 4.470 x 1.655 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 - 35KN - 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 35 kN with an ultimate load rating of 52.5 kN. It has a proof load of 43.5 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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