| Featured Space and Satellite Products this Week |
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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 has an output voltage in the range of 3.8-23.1 V and a power consumption of up to 188 W. The PPDH110-1PL has a design life of 5 years in LEO and combines the functions of power conditioning and data handling for the payload units. |
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| 3.3 V Star Tracker for Earth observation Applications | |
Star Tracker
from CubeSpace
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| CubeStar GEN 2 is a medium to high accuracy star tracker designed by CubeSpace for low power consumption, in a small form factor. It outputs quaternions directly and has both “lost in space” and tracking modes. It has an accuracy of 0.02-0.06° and a data update rate of 1 Hz. The CubeStar Gen 2 is ideal for Earth observation and communication applications. |
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| 17.7-20.2 GHz Ka-Band SATCOM Low Noise Amplifiers | |
SATCOM Amplifier System
from Orbital Research
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| The WB Ka LNA from Orbital Research is a SATCOM Amplifier System with a frequency range of 17.7-20.2 GHz and a low noise temperature of 120 K. This Ka-band amplifier system has a mass of 250 g and measures 111.5 x 41.3 x 31.9 mm. It is designed for various applications like satellite teleports and gateways, telemetry, tracking and command(TT&C), and airborne terminals. |
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| 1-6 GHz Low Noise Amplifier for Space Applications | |
RF Amplifier
from Teledyne e2v HiRel Electronics
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| The TDLNA002093SEP from Teledyne e2v HiRel Electronics is a Space Qualified RF Amplifier that operates from 1-6 GHz. This amplifier has a gain of 21 dB. It requires a maximum supply voltage of 6 V and has a maximum dissipated power of up to 1000 mW. The amplifier is ideal for satcom, military, distributed antenna systems, GPS receivers, and space applications. |
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| 9-14 GHz High Power Amplifier for Telecom and Space Applications | |
RF Amplifier
from ERZIA
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| The ERZ-HPA-0900-1400-34 from ERZIA is an RF Amplifier that operates in a frequency range of 9-14 GHz. This amplifier has a small signal gain of 32 dB and a gain flatness of +/- 2.0 dB. It has a saturated output power of 33-36 dBm and an input/output VSWR of 1.8:1. The amplifier is ideal for industrial/laboratory, satcom/telecom, space, aerospace, and military applications. |
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| 3.4-4.2 GHz C-Band Satellite Downconverter | |
Block Downconverter
from WORK Microwave
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| The VHBD-VSBD-VHBDR-VSBDR-C from WORK Microwave is a Block Downconverter that has an input RF frequency range of 3.4-4.2 GHz and an output frequency of 950-1750 MHz. This Ku-band block downconverter has an LO frequency of 5.15 GHz and a phase noise of up to -133 dBc/Hz. It has an impedance of 50 Ohms and an input/output return loss greater than 18 dB. |
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| 28-118 W Solar Arrays for 6U/12U CubeSats | |
Satellite Solar Panel
from Blue Canyon Technologies
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| The Solar Arrays 6U/12U from Blue Canyon Technologies is a Satellite Solar Panel with carbon fiber and honeycomb structures. It has an array power of 48-118 W and has a DC voltage of 17 or 34.1 V. It has standard arrays include 30 percent efficient cells with Frangibolt release mechanisms for minisatellites and magnetic dipole mitigation. It is suitable for CubeSats and minisatellites. |
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| Sponsored by PCB Directory | | |
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| Hollow Parallel Pre-stressed Actuator for Space Applications | |
Space Actuator
from Cedrat Technologies
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| The HPPA-8 from Cedrat Technologies is a Direct Piezo Actuator with a 8 mm diameter internal hole available for an optical function. It delivers a stroke of 8 µm with an operating voltage range of -20 V to -150 V. It has a mass of 21 g and has an outer diameter of 30 mm with a height of 25 mm. The actuator is ideal for optical delay line, refocussing and tuning of external laser cavity applications. |
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| Solar Array Drive Mechanism for NanoSats and SmallSats | |
Solar Array Drive Mechanism
from IMT
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| The IMT µSADA from IMT is a Solar Array Drive Mechanism developed for CubeSat platforms sized 6U/12U. It features a robust hold-down and release mechanism that supports CAN Bus interface and generates up to 118 W using space-qualified triple-junction solar cells. It has an average power consumption of 500 mW. It is ideal for nanosatellites and small satellites. |
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| 6 U Nanosatellite Bus for Earth Observation and Climate Monitoring | |
Satellite Bus & Platform
from SPACEMANIC
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| The Corvus 6U Nanosatellite Bus from SPACEMANIC is a Satellite Bus & Platform with a design life of up to 5 years. It has 3x and 6x configurable channels of 3.3, 5 and 12 V. It has a battery stored energy of 92 Wh which supports RS485, CAN and I2C interface. This platform requires a voltage supply of 12 v and has a power rating of up to 48 W. It has a payload mass of up to 7.5. |
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| High-Resolution Satellite Imaging Payload for Nano-Satellites | |
Satellite Camera
from L3Harris Technologies
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| The SPACEVIEW 24 (SV-24) from L3Harris Technologies is a High-Resolution Satellite Imaging Payload with an optical aperture of 0.24 meters. It delivers a ground sampling distance of 0.9–1.1 m at 500 km altitude, enabling sub-meter resolution for precision Earth observation. It is ideal for satellite constellations requiring rapid revisit times and actionable imaging intelligence. |
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| 12-18 GHz Coupler for Geostationary Satellites | |
Space Qualified Coupler
from CTech
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| The SemaLink Ku-OMUX WR 75 from CTech is a Space Qualified Coupler with an operating frequency of 12-18 GHz. It has an insertion loss of 0.5 dB and an isolation of 28 dB. It has a flight heritage with TÜRKSAT 6A satellite mission and supports WR 75 as data interfaces. The coupler has more than 15 years of lifetime and is fully space qualified for geostationary satellites. |
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| 104-177 L Propellant Tank for Spacecrafts | |
Spacecraft & Satellite Propellant Tank
from Orbital Propulsion Centre
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| The SURFACE TENSION TANK OST 31/0 from Orbital Propulsion Centre is a Spacecraft & Satellite Propellant Tank with a net tank volume of 104-177 L and a MEOP of 24.6 bar. It is constructed using Ti6AI4V STA (3.7164.7) material for the pressure vessel and Ti6AI4V (3.7164.1) for the suspension/ports. The propellant tank has been used on Globalstar project application. |
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| Coaxial High-Gain Pyramidal Horn Antenna | |
Satellite Antenna
from Scientific Microwave Corporation
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| The WR28 from Scientific Microwave Corporation is a Coaxial High-Gain Pyramidal Horn Antenna that operates from 26.5-40 GHz. It has an aluminum enclosure with an SMA female connector and a WR28 waveguide interface. This antenna is ideal for radar systems, satellite communication, wireless power transfer, anechoic chambers and radio astronomy applications. |
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| 1.1 mN Iodine Gridded Ion Thruster for Deep-Space Missions | |
Spacecraft Thruster
from Busek
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| The BIT-3 from Busek is a Spacecraft Thruster with a thrust value of 1.1 mN and a specific impulse of 2150 seconds. It has an innovative thruster gimbal capable of desaturating reaction wheels as part of the Attitude Control System (ACS). It has a thruster mass of 1.4 Kg with gimbals and measures 180 x 88 x 102 mm. This thruster is ideal for deep-space CubeSat missions. |
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