| Featured Space and Satellite Products |
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| Space-Qualified Rubidium Atomic Frequency Standard Clock | |
Space Qualified Atomic Clock
from Excelitas Technologies
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| The Rubidium Atomic Frequency Standard (RAFS) from Excelitas Technologies is a Space-Qualified Atomic Clock with an output frequency of 13.4 MHz and a maximum frequency stability of 2x10-12 (at 1 sec). It has a phase noise of -95 dBc and a return loss of greater than 20 dB. This atomic clock has harmonics of 50 dBc and a spurious signal range of -85 to -50 dBc. It is ideal for Global Navigation Satellite Systems (GNSS) applications. |
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| 13.75-14.50 GHz VSAT Terminal | |
VSAT Terminal
from Cobham Satcom
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| The Sailor 1000 XTR KU from Cobham Satcom is a VSAT Terminal with a receiver frequency range of 13.75 - 14.50 GHz and a transmitter frequency range of 10.70 - 12.75 GHz. It has a transmit gain of 41.6 dBi and a receive gain of 40.6 dBi. It offers linear X-Pol and Co-Po polarizations and is integrated with two multi-band LNB converters. It weighs 120 kg and is suitable for GNSS, Gyro, GPS, GLONASS, and Beidou applications. |
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| 200 V Radiation-Hardened Fast Recovery Rectifier | |
Space Qualified Diode
from STMicroelectronics
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| The STTH40200CHR from STMicroelectronics is a Space Qualified Diode with a forward current of 2 x 20 A and a repetitive peak reverse voltage of 200 V. The diode is assembled in a TO-254AA hermetic package and is screened to comply with the ESCC5000 specification. It has a radiation tolerance TID of up to 3 Mrad(Si) and is Single Event Effect tested up to 62.5 MeV.cm/mg (LET). The diode has a package mass of 9.4 g and is ideal for aerospace applications. |
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| Launch Vehicle Electromechanical Linear Actuator | |
Launch Vehicle Actuator
from Moog
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| The TVC Upper Stage Redundant (0.4 hp) from Moog is a Launch Vehicle Actuator with a horsepower of 0.4 hp and a stall load capacity of 3190 lbf. This actuator has a powerpoint of 2.18 in/sec (at 1100 lbf) and requires a supply voltage of 28 V. It has a null length of 23.25 inches (centered). The actuator is used to provide thrust vector control for launch vehicles and has been used in several launch vehicles such as Antares, Delta IV, Centaur, and Vega. |
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| SmallSat Power Conditioning and Distribution Unit | |
Power Conditioning and Distribution Unit (PCDU)
from Bradford Space
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| The SuperNova PCDU from Bradford Space is a Power Conditioning and Distribution Unit (PCDU) with a capacity of up to 1.5 kW. This PCDU is capable of interfacing between 28V nominal Li-Ion batteries, up to 80 V solar array sections, and a set of regulated and/or unregulated loads. It has a solar array power conversion efficiency of up to 95 % and a trickle charge current of 2 A. It is ideal for LEO and deep space applications. |
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| 100V, 60A Enhancement Mode GaN Power Transistor | |
GaN Power Transistor
from Renesas Electronics
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| The ISL73023SEH from Renesas is a GaN Power Transistor with a drain-source voltage of 100 V and a gate threshold voltage of 0.7-3 V. It has a continuous drain current of up to 60 A with a low drain-source on-resistance of 5-12 mO, a total gate charge of 14-25 nC and an input capacitance of 1500 pF. It is ideal for high-reliability applications such as switching regulation, motor drives, relay drives, inrush protection, and downhole drilling. |
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| Three-Axis Magnetometer for Satellites | |
Magnetometer
from NewSpace Systems
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| The NMRM-Bn25o485 from NewSpace Systems is a Magnetometer with a measurement range of +/- 60 µT and a resolution of less than 8 nT. This magnetometer has a noise density of less than 16 nT rms/Hz. It is suitable for the calculation of magnetorquer rods control torque levels, attitude determination sensors when used with an IGRF reference model, and angular rate determination sensor by comparing successive measurements. |
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| Ka-Band SATCOM BUC | |
SATCOM Block Up Converter
from Wavestream Corporation
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| The WBAN-050G01-0005 from Wavestream Corporation is a SATCOM block-up converter with an IF frequency range of 950 - 1950 MHz. It has a frequency reference of up to 5 dB and a small gain signal of 62.5 dB. This Ka wideband BUC has an output saturated power of 47 dBm and a linear power of 25 W. It requires a DC power supply of 20 - 56 V, supports RS- 482 and ethernet interface and operates on LEO, GEO, and MEO Ka-band satellites. |
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| Sponsored by GLOBAL MILSATCOM | | |
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| 100 V Rad-Hard Solid-State Relay | |
Space Qualified Solid State Relay
from Infineon Technologies
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| The RDHA701FP10A8QK from Infineon Technologies is a Space Qualified Solid State Relay with a maximum output voltage of 100 V and an output current of 1.3 A. This relay requires an input supply voltage of 10 V and has a power dissipation of up to 5.5 W. It has an output capacitance of 145 pF and a thermal resistance of up to 18 Degrees C/W. This relay is available in a 64-pin flatpack and comes in a hermetically sealed package. |
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| 80-125 MHz OCXO for Space Applications | |
Space Qualified Oscillator
from AXTAL GmbH & Co. KG
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| The AXIOM6060 from AXTAL GmbH & Co. KG is a Space Qualified Oscillator with a frequency range of 80-125 MHz. It has a spurious value of -80 dBc and harmonics of -35 dBc. It has a frequency stability of ±50 ppb (vs. operating temperature range), a current consumption of up to 600 mA. a low phase noise of up to -170 dBc/Hz. The oscillator has a mass of 130-200 g and measures 60 x 60 x 30. It is suitable for GEO and LEO missions. |
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| 6.725-7.025 GHz Test Loop Translator for SATCOM Applications | |
Test Loop Translator
from GeoSync Microwave
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| The TRE-6.8-4.6 from GeoSync Microwave is a Test Loop Translator with an input frequency range of 6.725-7.025 GHz and an output frequency range of 4.5-4.8 GHz. This test loop translator has an LO frequency of 2.225 GHz and an impedance of 50 Ohms. It has a return loss of 18 dB and a noise figure of up to 25 dB. The test loop translator has a phase noise of up to -110 dBc/Hz and supports RS485 and RS422 serial interfaces. |
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| Gridded Ion Thruster for SmallSats | |
Spacecraft Thruster
from ThrustMe
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| The NPT30-I2 from ThrustMe is a Gridded Ion Thruster that has a thrust of 0.0003 to 0.0011 N. This spacecraft thruster has a mass of 1.2-1.7 Kg and a specific impulse of up to 2400 sec. It has a power consumption of up to 35-65 W and requires a supply voltage of 12-28 V. This thruster is designed for SmallSats and supports I2C, and CAN interfaces. It is available in two dimensions: 1U (96 x 96 x 113 mm) and 1.5U (93 x 93 x 155 mm). |
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| DC - 50 GHz Wideband Analog Attenuator | |
Space Qualified Variable Attenuator
from Qorvo
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| The TGL4203 from Qorvo is a Space-Qualified Variable Attenuator with a variable attenuation range of 17 dB. It has a typical insertion loss of 2 dB and a return loss of 15 dB. This analog attenuator has a broadband response of greater than DC to 50 GHz and an attenuation control voltage range of -5 to +0.5 V. This wideband attenuator is ideal for applications such as point-to-point radio, fiber optic, and wideband military and space. |
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| Onboard Computer for Microsat Missions | |
Satellite On-Board Computer (OBC)
from GomSpace
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| The NanoMind A3200 from GomSpace is a Satellite On-Board Computer (OBC) that is based on a high-performance AVR32 MCU with a clock frequency of 8-64 MHz. This OBC board carries a 128 MB NOR serial flash and a 512 KB built-in flash. It has a 32 MB SDRAM and 32 kB FRAM for persistent configuration storage. It supports the CAN and I2C interface. This OBC is ideal for mission-critical space applications and CubeSat or nano-satellite missions. |
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| C-Band Transceiver for VSAT Networks | |
SATCOM Transceiver
from Amplus Communication
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| The AM-9444 from Amplus Communication is a SATCOM Transceiver with a transmit frequency range of 5850-7025 MHz and a receive frequency range of 3625-4800 MHz. This transceiver has a Tx gain of 80-83 dB and an Rx gain of 45 dB. It has a phase noise of up to -93 dBc/Hz and a maximum spurious of -55 dBc. It has a mass of 23 Kg and measures 495 x 265 x 215 mm. The transceiver is ideal for crucial VSAT networks. |
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