| Featured Space and Satellite Products this Week |
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| 0.22-10 µH Space Qualified Tin / Lead Inductor | |
Space Qualified Inductor
from Vishay
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| The IHLP-3232CZ-L1 from Vishay is a Space Qualified Inductor with an inductance range of 0.22-10 µH and an inductance tolerance of +/- 20 %. This shielded inductor has a saturation current of 8.2-43 A and a heat rating current of 4.7-32 A. It is suitable for various applications such as high-current POL converters, high-current power supplies, battery-powered devices, DC/DC converters in distributed power systems, and DC/DC converters for FPGAs. |
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| 4 W Ka-Band Block Upconverter | |
Block Upconverter
from Norsat
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| The ELMTBKA004 from Norsat is a Block Upconverter with a transmit frequency range of 30.0-30.5 GHz and an IF frequency range of 950-1450 MHz. This BUC has an LO frequency of 29.05 GHz and a linear gain of 53-63 dB. It has a gain flatness of less than 4.0 dB p-p (full band) and a saturated output power of 36.5 dBm. The BUC has a minimum output power P1dB of 36 dBm and a maximum phase noise of up to -95 dBc/Hz at 100 kHz. |
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| SmallSat Mass Memory and Communications Protocol Unit | |
Satellite On-Board Computer (OBC)
from AAC Clyde Space
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| The SIRIUS TCM LEON3FT from AAC Clyde Space is a Satellite On-Board Computer (OBC) with a real-time operating system that runs on a 32-bit LEON3FT fault-tolerant processor. This command and data handling system consists of an onboard computer (Sirius OBC) and a combined mass memory with a CCSDS stack (Sirius TCM). The OBC is designed and qualified for five years of operation in low-earth orbit and is ideal for advanced satellite missions. |
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| 470-500 kOhm Space Qualified Chip Resistor | |
Space Qualified Resistor
from TT Electronics
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| The RM1206 from TT Electronics is a Space Qualified Resistor with a resistance range of 470-500 kOhm and a tolerance of +/- 0.1-10 %. This resistor has a rated voltage of 100 V and a rated power of 100 mW. It has a temperature coefficient of resistance of 300 ppm/degrees C and is qualified to MIL-PRF-55342 Space Level T. The chip resistor is designed using TaN film technology. It is ideal for all high-reliability military and space applications. |
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| 5.925-6.425 GHz Outdoor Mounted Frequency Band Translator | |
Test Loop Translator
from GeoSync Microwave
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| The TLE-6.175-INV from GeoSync Microwave is a Test Loop Translator with an input frequency range of 5.925-6.425 GHz and an output frequency range of 0.95-1.45 GHz. This test loop translator has an LO frequency of 7.375 GHz and an impedance of 50 Ohms. It has a gain of 17-23 dB and a minimum spurious of 65 dBc (signal related). It is ideal for applications requiring frequency translation with a minimum amplitude and group delay distortion. |
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| 5 V Tolerant Radiation Hardened 4 Mbit SRAM | |
Space Qualified Memory
from Microchip Technology
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| The AT60142HT from Microchip Technology is a Space Qualified Memory that is organized as 512K x 8 bits. This CMOS static RAM has an operating voltage of 3.3/5 V and low power consumption of 3.3 mW (standby) and up to 610 mW (active max at 17 ns). It has a fast access time of 15-17 ns over the full military temperature range. It is ideal for fast computing and low-power consumption applications such as aerospace electronics, portable instruments, or embarked systems. |
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| DC to 40 GHz Space Qualified Subminiature Connector | |
Space Qualified RF Connector
from Rosenberger
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| The 19-000-000_TD from Rosenberger is a Space Qualified RF Connector with a frequency range of DC to 40 GHz and an impedance value of 50 ohms. This connector has a return loss of 14-23 dB and an insertion loss of up to 0.6 dB. It has an insulation resistance of greater than 5 GOhms and a center contact resistance of less than 6 mOhms. It is ideal for lowest to highest mechanical load applications such as 5G mobile telecommunications, test, measurement, and aerospace. |
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| 4 Channel Satellite Link Emulator for Payload Testing | |
Satellite Link Emulator
from dBm Corporation
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| The ACE9600 from dBm Corporation is a Satellite Link Emulator with a center frequency of 1125 MHz and a 1 dB RF bandwidth of 600 MHz. It has an in-band spurious suppression of -55 dBc and a VSWR of less than 1.5:1. The emulator is ideal for applications such as Earth terminal testing, satellite payload testing, satellite system integration test beds, mobile transceiver testing, UHF/VHF radio testing, UAV testing, and atmospheric scintillation (time dispersive delay) modeling. |
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| Cold Gas Thruster for Customized Propulsion Systems | |
Spacecraft Thruster
from Dawn Aerospace
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| The B1 from Dawn Aerospace is a Cold Gas Thruster with a thrust range of 0.49-1.35 N. This thruster utilizes nitrous oxide (N2O) and propylene (C3H6) green propellants and has a specific impulse of 248 sec. It has a pulse frequency of 4 Hz and a minimum impulse bit of 1.4 mN.s (Cold gas). The thruster uses a spark-based igniter. The thruster can achieve 6DOF satellite control and is also suitable for rendezvous and proximity operations. |
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| -60 V Radiation Hardened P-Channel MOSFET | |
Space Qualified MOSFETs
from Infineon Technologies
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| The IRHLUBC7970Z4 from Infineon Technologies is a Space-Qualified MOSFET with a drain-to-source breakdown voltage of -60 V and a continuous drain current of -0.53 A. This radiation-hardened MOSFET has a gate-to-source voltage of +/- 10 V and a gate threshold voltage of -2 to -1 V. It has a pulsed drain current of -2.12 A and a drain-to-source resistance of 1.4 Ohms. The MOSFET is ideal for applications such as DC-DC converters and motor controllers. |
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| 5 W Ka-Band Portable Satellite Antenna Terminal | |
Satellite Terminal
from DataPath
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| The CCT120-GX from DataPath is a Satellite Terminal that has a transmit frequency range of 29.0-30.0 GHz and a receive frequency range of 19.2-20.2 GHz. This terminal has a minimum EIRP of 54 dBW and a G/T of 19.3 dB/K. It has a wide azimuth travel range of +/- 90 degrees and an elevation range of 10-90 degrees. The terminal requires a power supply of 85-265 V AC. It is wideband Ka capable, ARSTRAT (WGS) compliant, and LEO and MEO (Multi-Orbit) capable. |
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| 218 L Propellant Tank for Spin Stabilized Spacecraft | |
Spacecraft & Satellite Propellant Tank
from Orbital Propulsion Centre
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| The T11-0 from Orbital Propulsion Centre is a Spacecraft & Satellite Propellant Tank with a net tank volume of 218 L and a maximum expected operating pressure of 22 bar. This propellant tank is compatible with MON propellant and pressurant gases such as helium and nitrogen. It has a proof pressure of 27.5 bar and a burst pressure of 33 bar. The propellant tank has been used on Meteosat Second Generation satellites and is suitable for spin-stabilized spacecraft. |
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| DC-42.5 GHz Wire Bondable Chip Termination | |
Space Qualified RF Termination
from Smiths Interconnect
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| The CT0404ALN1WB1 from Smiths Interconnect is a Space Qualified RF Termination with a frequency range of DC-42.5 GHz. This chip termination has a nominal impedance of 50 Ohms and a VSWR of 1.25:1. It has a power rating of up to 5 W and a peak power of up to 50 W. The termination is suitable for applications such as amplifier circuits, isolators, transmit/receive modules, up/down converters, instrumentation, satellite communications, radar, and broadcast. |
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| X-Band Low-Noise Block Down Converter for Transportable Applications | |
SATCOM Low Noise Block
from Comtech EF Data
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| The X-Band Low-Noise Block from Comtech Satellite Network Technologies is a SATCOM Low Noise Block with an input frequency range of 7.25-7.75 GHz and an output frequency range of 950-1450 MHz. This LNB has a gain of 50-60 dB and a 1 dB compression point of 10 dBm. It meets the system requirements for commercial and military geosynchronous satellites worldwide and its compact design makes it ideal for transportable applications and severe environments. |
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| Biaxial Gimbal Assembly for Antenna Positioning | |
Antenna Pointing Mechanism
from Moog
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| The Type 33 Biaxial Gimbal from Moog is an Antenna Pointing Mechanism with an output torque of 17 N-m and an output step angle of 0.009375 Degrees. This two-axis antenna pointing assembly has a powered holding torque of 34 N-m and an unpowered holding torque of 9 N-m. It can incorporate a wide range of options such as launch locks, caging mechanisms, cable management systems, position sensors, and waveguide brackets/ mounting. |
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