| Featured Space and Satellite Products |
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| 5000 Ohms GSFC Space Qualified Thermistor | |
Space Qualified Temperature Sensor
from TE Connectivity
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| The 44906 from TE Connectivity is a Space-Qualified Temperature Sensor with a resistance of 5000 ohms and an interchangeability of +/- 0.1 °C (0°C to 70°C). It has a thermally conductive epoxy coating that exhibits less than 0.66% TML and 0.10% WVR. This GSFC S311-P18-01S7R6 qualified thermistor is ideal for extended space, low and mid-range temperature, tight tolerance instrumentation and applications requiring sensing small temperature changes. |
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| 4-16 GHz GaAs Surface Mount MMIC IQ Mixer for Band Shifting | |
Space Qualified RF Mixer
from Marki Microwave
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| The MMIQ-0416LSM-2 is a GaAs MMIC mixer for low-frequency applications with an RF/LO frequency from 4-16 GHz and an IF frequency from 0-6 GHz. The mixer has an IP3 of 4-16 dBm and an image rejection of up to 40 dB. It has a banded performance is possible at LO drive as low as +4dBm. It is ideal for Single Sideband and Image Rejection Mixing, IQ Modulation/Demodulation, Vector Amplitude Modulation, and Band Shifting applications. |
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| Non-Pyrotechnic Space Vehicle Separation System | |
Separation System
from Rocket Lab
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| The 2003336B from Rocket Lab is a Separation System that is designed to separate space vehicles from launch vehicles. The separation system has a total mass of 3000 Kg and has integrated springs, switches and connectors that streamline mission design. It requires a supply voltage of 24-32 V. It has a deployed life of 20 years and is suitable for commercial, government, private and university customers for LEO, GEO and interplanetary orbits. |
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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 of small and nanosatellites. The receiver is suitable for satellite constellations such as GPS, GALILEO, BEIDOU, QZSS, GLONASS, NAVIC and SBAS. It requires an input DC voltage of 3.3 V and has a power consumption of 0.6-1.1 W. It is ideal for data monitoring, navigation algorithms like orbit propagation and clock synchronisation. |
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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. The converter is designed to support the demanding requirements of modern satellite transmission applications and is ideal for systems where an accurate phase relationship is required between two converter channels, as in the case for mono-pulse tracking system down conversion. |
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| 4 MP Optical Imager for Nano Satellites | |
Satellite Camera
from AAC Clyde Space
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| The IM200 from AAC Clyde Space is a Satellite Camera that comes with a 4-megapixel resolution. It has a pixel scan rate above 30 MP/s and has a very low power consumption of less than 700 mW. It supports TTL UART interface for command and USB, RS422, RS485, and I2C interface as optional. This imager has a radiation tolerance qualified up to 9 krad (Si). It measures 29 x 29 x 70.7 mm. The imager is suitable for applications on larger satellite platforms. |
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| Accelerometer for Solar Tracking/Pointing Systems | |
Space Qualified Accelerometer
from Solar MEMS
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| The Sensor MASS-X from Solar MEMS are space-qualified accelerometers that integrate a 3-axis accelerometer and a high-precision sun sensor designed to measure the incidence angle of sun rays, direct normal irradiance (DNI) solar radiation along with the azimuth and elevation positions of the device. These sensors are ideal for applications such as heliostats, solar tracking/pointing systems, sun radiation monitoring and attitude control using light sources. |
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| Sponsored by PCB Directory | | |
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| Water-Powered Electrothermal Spacecraft Thruster | |
Spacecraft Thruster
from SteamJet Space Systems
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| The Steam Thruster One from SteamJet Space Systems is a Spacecraft Thruster with a nominal thrust of 5-20 Nm and a specific impulse of 172 s. It has a high total impulse of 1200 Ns and a thrusting power consumption of 19.9 W . It has a wet mass of 1700 g and a propellant mass of 700 g. This electrothermal propulsion technology is requires a DC supply voltage of 17-33 V and supports RS422, TTL and UART interfaces. It is ideal for CubeSats and Small Satellites. |
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| 8.025-8.4 GHz C-band Transmitter for Space Applications | |
Space Transmitter
from Cubecom
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| The XTX G2 from Cubecom is a Space Transmitter that has a frequency range of 8.025-8.4 GHz and has a data transmitting rate of 250 Mbps. It has a channel spacing of 1 MHz and has a symbol rate of 5-50 Msps. It requires an input voltage of 7-20 V and has a power consumption of 15 W. This space-qualified transmitter has a total mass of 137 g and measures 96 x 90 x 13 mm in dimension. It is designed with a Cubesat Kit PC/104 form factor for Nanosatellite missions. |
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| Non-Pyro Satellite Separation System For Nanosatellites | |
Separation System
from Antrix Corporation Limited
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| The INLS 1U from Antrix Corporation Limited is a satellite separation system designed for 1 kg class nanosatellites that is housed inside a rectangular enclosure and secured by a swinging door. It requires a power supply of 2.4 V. The separation system has a separation time of 5 seconds and has a satellite size of 100 × 100 × 113.5 mm. It has demonstrated proven flight heritage, having successfully deployed STUDSAT on PSLV-C15 and SWAYAM on PSLV-C34. |
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| GNSS Simulators for Navigation Applications | |
GNSS Simulator
from WORK Microwave
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| The Xidus-6HU from WORK Microwave is a GNSS Simulator that operates at a frequency range of 1110-2540 MHz and has an accuracy of ±0.3 dB. It features a flexible configuration using GUI/Remote commands that has a simulation rate up to 1000 Hz. It requires an AC operating voltage of 100-240 V. It measures 447.5 x 266.7 x 500 mm and is ideally used in research and development of GNSS receivers, including aviation, maritime and other navigation applications. |
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| 8-20 Degrees Sun Sensor Simulator for Satellite Systems | |
Sun Sensor Simulator
from SPUTNIX
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| The SXL-SUNSIM-01 from SPUTNIX is a Sun Sensor Simulator with a beam angle of 8-20 deg and a maximum light spot diameter of 600 mm. It provides an illumination of about 90,000 lux at a distance of 1.5 meters and has an illumination power density of 1400 W/m². It requires a power supply of 220 V. It does not support focus length and beam angle adjustment. This fixed light source illuminates the test object simulating solar radiation in the optical frequency range. |
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| 8-8.4 GHz Hemispherical Antenna Pointing Mechanism | |
Antenna Positioning Mechanism
from Airbus
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| The LEO X-Band from Airbus is an antenna pointing mechanism designed for hemispheric coverage in low Earth orbit communications. It offers a pointing accuracy of less than 0.5° and a rotational velocity under 10°/s. It has an independent 2-axis movement with full azimuth rotation and variable elevation that uses a geared stepper motor drive and contactless rotary joints for RF signal transfer. It has a mass of less than 12.5 kg and a moving envelope of 95 x 82 cm. |
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| Reconfigurable Computer for Space Payload Processing | |
Satellite On-Board Computer (OBC)
from SEAKR Engineering LLC
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| The RCC 5 from SEAKR is a fifth-generation reconfigurable computer that is built on three Virtex-5 FX-130T FPGAs with extended 6U cPCI module integrates high-speed SERDES I/O and on-board configuration storage with an optional scrubber for enhanced reliability. This OBC has a mezzanine interface that includes 24 MGT SERDES channels and 339 GPIO lines enabling extensive system integration. It is designed for advanced space payload processing applications. |
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