| Featured Space and Satellite Products |
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| 8.4-12.5 GHz Passive GaAs MMIC Bandpass Filter | |
Space Qualified RF Filter
from Marki Microwave
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| The MFBA-00004BH from Marki Microwave is a Passive MMIC Bandpass Filter with a passband from 8.4-12.5 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 and has a 2.92 mm (female) connector. |
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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. |
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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 has a mass of 3.5 Kg and measures 110 x 240 x 170 mm. |
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| Multi-Frequency GNSS Receivers for Space Navigation | |
GNSS Receiver
from Rakon Limited
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| The GNSS DB from Rakon Limited is a GNSS Receiver with multi-band and multi-constellation support designed for small and nanosatellites. This receiver has a position accuracy of 1.2 m and a velocity accuracy of less than 3 cm/s RMS. It requires an input DC voltage of 3.3 V and has a power consumption of 0.6-1.1 W. The receiver measures 55 x 41 x 16 mm. It is ideal for data monitoring, navigation algorithms like orbit propagation and clock synchronisation. |
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| Surface Mount Diplexer for GPS Applications | |
Space Qualified RF Diplexer
from Mini Circuits
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| 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 low insertion loss of 0.6-2.9 dB and return loss of 6-17 dB. This RoHS compliant diplexer is ideal for applications such as satellite systems, cellular, GPS, multiband communication systems and WCDMA networks. |
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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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| 26.5 V DPDT Full Size General Purpose Signal Relay | |
Space Qualified Solid State Relay
from TE Connectivity
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| The B07D111BC4-0006 from TE Connectivity is a Space Qualified General Purpose Power Relay that operates with a coil voltage rating of 26.5 VDC and has a maximum coil power of 2.341 W. It has a non-polarized monostable coil magnetic system with a coil resistance of 300 ohms and has a contact rating of 10 A. The relay is hermetically sealed and has a configuration feature of 2 Form C DPDT-CO contact arrangement. |
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| Sponsored by Marki Microwave | | |
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| Reaction/Momentum Wheel for LEO Orbits | |
Reaction Wheel
from SITAEL
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| The Reaction/Momentum Wheel (RMW) from SITAEL is an attitude control device that provides a high stall torque and has a control torque of up to 10 mNm and can store an angular momentum of up to 0.4 Nms. The system supports control via the RS232 interface, with an option for a redundant CAN bus communication port. It weighs up to 1100 g and measures 120 x 100 x 130 mm. The reaction wheel is designed for Low Earth Orbit (LEO) satellites. |
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| 16 W Ka-band Block Upconverter for SATCOM Applications | |
Block Upconverter
from Norsat
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| The ELMTBKA016 from Norsat is a 16W Ka-band Block Upconverter with a transmit frequency range of 29-30 GHz (Commercial) and 30-31 GHz (Military). It supports an IF frequency range of 950–1950 MHz. It offers gain flatness under 4.0 dB and has a saturated output power of 42 dBm. This BUC has a minimum output power P1dB of 34 dBm and has a phase noise reaches up to -103 dBc/Hz at 1 MHz. It has an output spurious value below -55 dBc. |
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| Multi-Band Tactical Deployable Earth Terminal | |
Satellite Terminal
from Gilat Satellite Networks
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| The DKET 3400 Series Ku-Band from Gilat Satellite Networks is a Multi-Band Tactical Deployable Earth Terminal that operates over a Ku-band uplink frequency range of 13.75–14.50 GHz and a downlink range of 10.7–12.75 GHz. It supports customer-specified 4RU expandable modems and offers up to 54 RU rack space. This terminal is ideal for secure, high-capacity and rapidly deployable satellite communications for military and commercial missions. |
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| 4 MP Monochrome Satellite Camera for Space Applications | |
Satellite Camera
from 3D Plus
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| The 3DCS04M110944 from 3D Plus is a Satellite Camera for space applications such as monitoring and navigation for spacecrafts and landers. This camera features 4 MPixels CMOS sensor module (Mono or RGB) with 2048 x 2048 active pixels (5.5 µm). It operates at an average power consumption of less than 2 W and supports up to 6 full-resolution frames per second in burst mode and 1.5 frames per second in continuous mode via SpaceWire. |
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| Power Control and Distribution Unit for SmallSats | |
Power Conditioning and Distribution Unit (PCDU)
from VECTRONIC Aerospace GmbH
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| The VPCDU-1 by VECTRONIC Aerospace is a highly integrated Power Control and Distribution Unit specifically designed for small satellite applications. It manages the spacecraft's entire power supply sourcing power from the solar array and battery to distribute it to all subsystems and payloads. It incorporates 3 independent interfaces for solar arrays supporting a wide input voltage range up to 60 V and 3 independent battery charge regulation channels. |
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| Payload Data Handling System for Nano and Micro Satellites | |
Payload Data Handling System
from Kongsberg NanoAvionics
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| The PAYLOAD CONTROLLER 1.5 from Kongsberg Nano Avionics is a Payload Data Handling System that serves as the interface between the satellite’s payload and its data storage unit in micro and nanosatellite platforms. It offers dual 512 kB FRAM modules via SPI for changing data storage frequently. It is supported by parallel NAND memory and an integrated TRC. It features three PWM-controlled H-bridges and multiple outputs for precise actuator control. |
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| O.8 V Space-Qualified Silicon Bypass Diode | |
Space Qualified Diode
from AZUR SPACE
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| The HNR 002576-00-03 from AZUR SPACE is a space-qualified silicon diode engineered to protect individual multi-junction space-grade solar cells from reverse current damage. It offers a forward voltage of up to 0.8 V. It has an n-side that includes thermal oxide at the edges for enhanced insulation and the p-side is fully covered to ensure optimal conductivity and protection. It weighs around 30 mg and is available in a package that measures 10.9 × 10.9 mm. |
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| 222 L Monopropellant Diaphragm Tank for Spacecrafts | |
Spacecraft & Satellite Propellant Tank
from MT Aerospace
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| The PTD-222 from MT Aerospace is a Spacecraft & Satellite Propellant Tank with a total volume of 222 L and a maximum expected operating pressure of 24.5 bar. It has a tank dry mass of 17.08 kg and a maximum propellant mas of 184 kg. The propellant tank has a proof pressure of 36.8 bar. It is compatible with hydrazine propellant and pressurant gases such as helium and nitrogen. It measures 607.75 x 1.022 mm with polar mounting tabs. |
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