| Featured Space and Satellite Products |
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| CubeSat Solar Array | |
Satellite Solar Panel
from AAC Clyde Space
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| The PHOTON-TD from AAC Clyde Space is a Satellite Solar Panel with a power generation capacity of up to 9 W. This solar panel uses XTJ Prime solar cells having an efficiency of 30.7% and features a 4 mil anti-reflective coated cover glass. It uses an aluminum support structure. The panel is designed to fit within the majority of CubeSat deployment mechanisms and is used to provide optimized power generation from any side of the satellite. |
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| Space Qualified Bandpass Filter | |
Space Qualified RF Filter
from Mercury Systems
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| The Ku1960 from Mercury Systems is a Space Qualified RF Filter with a passband frequency range of 17300-17700 MHz. This filter has a maximum insertion loss of 1.0 dB and a VSWR of 1.3:1. It has a rejection of 40 dB at 17800 MHz and an insertion loss flatness of 0.25 dB. The filter features a cavity design and a static notch. It has a mass of 0.2 lb. The filter is ideal for communication satellites and test equipment. |
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| 1.3 Meter Tri-band Flyaway VSAT | |
VSAT Terminal
from L3Harris Technologies
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| The HAWKEYE 4 LITE from L3Harris Technologies is a VSAT Terminal with a transmit frequency range of 7.90-8.40 GHz (X-band), 13.75-14.50 GHz (Ku-band), and 29.0-31.0 GHz (Ka-band). This terminal has a receive frequency range of 7.25-7.75 GHz (X-band), 10.95-12.75 GHz (Ku-band), and 19.2-21.2 GHz (Ka-band). The VSAT terminal is designed using industry-leading Viewsat-E GUI and GATEKEEPER interference excision technology. |
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| Fiber Optic Gyro Inertial Measurement Unit | |
Inertial Measurement Unit
from EMCORE Corporation
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| The CIRUS-A from EMCORE Corporation is an Inertial Measurement Unit with a gyro bias stability of 0.0001 degrees/hr and a scale factor stability of +/- 2 ppm. The IMU delivers state-of-the-art, strategic-grade performance for platform stabilization, pointing applications, missile guidance systems, vehicle/platform navigation, and northfinder applications for missile, space, sensor, ground, air, and marine applications. |
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| 0.5 mOhm D-Sub Connectors for Spaceflight Applications | |
Space Qualified RF Connector
from Positronic
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| The MCBX Series from Positronic is a Space Qualified RF Connector with an insulation resistance of 50 Gohm and an initial contact resistance of 0.5 mohm. This connector has a working voltage of 300 V and a proof voltage of 1000 V. It meets or exceeds the performance requirements for NASA Goddard GSFC-311 and MIL-DTL-24308. The connector has a mechanical durability of 500 cycles and is ideal for military, aerospace, and spaceflight applications. |
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| Ka-Band 40 W SATCOM Block Up Converter | |
SATCOM Block Up Converter
from ACORDE
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| The ACTX-Ka40W-Ex-V4 from ACORDE is a SATCOM Block Up Converter with an input frequency range of 950-2000 MHz and an output frequency range of 27.5-31.0 GHz. This BUC has a minimum gain of 65 dB and a saturated power of 46 dBm. The BUC is designed for harsh environmental conditions and is ideal for professional and military satellite communication systems such as ground, SOTP, SOTM, and maritime. |
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| Piezoelectric Rotary Stage for Space Applications | |
Space Actuator
from PHI Drive
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| The AG-HTS from PHI Drive is a Space Actuator with a travel range of +/- 360 degrees. It has a no-load speed of 0.04 RPM and a stall torque of 9 Nm. This actuator uses a piezo stack-type drive with a capacitance of 760 nF. It has an operating frequency range of 0-40 Hz. The actuator uses Inconel 718 material for the core, rotating ring, and stator ring. It is particularly suited for aerospace, military, and space applications. |
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| 25 W Ku-Band SATCOM Transceiver | |
SATCOM Transceiver
from AnaCom, Inc
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| The Anasat Ku-band 25W from AnaCom is a SATCOM Transceiver with a Tx output frequency range of 13.75-14.5 GHz and an Rx input frequency range of 10.95-12.75 GHz. This transceiver has a Tx gain of 75 dB and an Rx gain of 75-100 dB. It has a 1-dB compression point of 44 dBm and a noise figure of 1-2 dB. The transceiver requires an input power supply of 100-250 V AC and has a power consumption of up to 300 VA. |
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| 600 V Radiation Hardened Solid State Relay | |
Space Qualified Solid State Relay
from Modular Devices
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| The 53804 from Modular Devices is a Space Qualified Solid State Relay that requires a bias voltage of 4.7-5.25 V and a command current of 0.1-2.0 mA. It has a contact current rating of 10-15 A and a contact voltage rating of 600-1000 V. This relay has a contact resistance of 0.15-0.4 ohm, a power dissipation of 20-30 W, and an energized delay time of 10-30 µs. The 53804 relay is ideal for military and aerospace applications. |
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| Solar Array Drive Assembly for SmallSats | |
Solar Array Drive Mechanism
from Moog
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| The Small Satellite Solar Array Drive Assembly from Moog is a Solar Array Drive Mechanism that has an output torque of 50 lbs-in. This mechanism has an output step size of 0.018 degrees and a cycle life of 90,000 revs of output. It requires an operating voltage of 22 VDC and has a power consumption of 10 W. It is capable of low-earth orbit operations. The mechanism is an ideal power solution for positioning solar array panels. |
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| 12-50 V Space-Qualified DC-DC Converter | |
DC to DC Converter
from Crane Aerospace & Electronics
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| The MCH2805S from Crane Aerospace & Electronics is a DC-DC Converter with an input voltage range of 12-50 V and an output voltage of 5 V. This converter has an output power of 1.5 W and an efficiency of up to 77 %. The converter has an input/output capacitance range of 100 - 170 pF and a switching frequency of 370 kHz. It is designed for harsh radiation environments and is ideal for aerospace, military, and space applications. |
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| 550 W Ka-Band Antenna Mount HPA | |
SATCOM Amplifier System
from Spacepath Communications
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| The STA5555P from Spacepath Communications is a SATCOM Amplifier System with a frequency range of 27.5-31 GHz. This amplifier system has a gain up to 70 dB and an output TWT power of 57.4 / 54.7 dBm. It has an input/output VSWR of 1.3:1 and a noise power of -70 dBW/4KHz (transmit band) and -150 dBW/4KHz (receive band). The amplifier system has a spurious of less than -60 dBc and a phase noise of up to - 50 dBc. |
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| Reaction Wheel Unit for Satellites | |
Reaction Wheel
from Bradford Space
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| The W18 from Bradford Space is a Reaction Wheel that consists of a Wheel Drive Electronics Box and a Reaction Wheel Assembly. This reaction wheel unit has a momentum storage of 18 Nms and a maximum operational speed of 4000 RPM. It has a maximum gross torque of 0.265 Nm and a static imbalance of 0.5 g.cm. It has flown on several successful missions such as SOHO, RadarSat, Seastar, and Olympus. |
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| 43.9-44.5 GHz RF Test Loop Translator | |
Test Loop Translator
from MICRONICS
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| The MCS-TLT-4419-08AC from MICRONICS is a Test Loop Translator with an input frequency range of 43.9-44.5 GHz and an output frequency range of 19.1-19.7 GHz. This test loop translator has an LO frequency of 24.8 GHz and a gain of -10 to 0 dB. It has a noise figure of 18 dB and a phase noise of -80 dBc (at 100 kHz). The translator has an input/output VSWR of 2:1. It is ideal for satellite communication applications. |
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| 250 V Radiation Hardened Power MOSFET | |
Space Qualified MOSFETs
from Infineon Technologies
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| The IRHLQ7S7214 from Infineon Technologies is a Space Qualified MOSFET with a drain-to-source breakdown voltage of 250 V and a gate-to-source voltage of +/- 10 V. This radiation-hardened MOSFET has a continuous drain current range of 1.6-2.6 A and a pulsed drain current of 10.4 A. It is ideal for applications such as DC-DC converters and motor drives and provides a simple solution to interfacing CMOS and TTL control circuits. |
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