| Featured Space and Satellite Products |
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| 30000 Ohms GSFC Space Qualified Thermistor | |
Space Qualified Temperature Sensor
from TE Connectivity
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| The 44910 from TE Connectivity is a Space-Qualified Temperature Sensor with a resistance of 30000 ohms and a tolerance of ± 0.1 Deg C (0°C to 70°C). It has a beta value of 3943 K and a beta tolerance of 0.4 %. This temperature sensor is ideal for extended space applications, low and mid-range temperature applications, tight tolerance instrumentation, and applications requiring sensing small changes in temperature and outgassing requirements. |
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| Earth/Horizon Sensor for Nanosatellites | |
Earth/Horizon Sensor
from CubeSpace
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| The CubeSense Gen 1 from CubeSpace is a Earth/Horizon Sensor that has an accuracy of 0.2° and with a field of view of 170°. It has a maximum slew rate of 10°/s and has an output data rate of 2 Hz. This CMOS-based sun sensor requires a supply voltage of 3.3 V and has a peak power value of 200mW. The earth/horizon sensor has a mass of 30 g and measures 41.7 x 17.7 x 22.9 mm. It is ideal for CubeSats and nano-satellite missions ranging from 2U-16U. |
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| GNSS Receiver for Accurate Muzzle Velocity Testing | |
GNSS Receiver
from ReliaSat
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| The W-x4RX-SM-9296 from ReliaSat is a GNSS Receiver with an RF frequency range of 92-96 GHz and IF frequency range of 2-6 GHz. It is ideal for highly accurate muzzle velocity testing and missile guidance systems, suitable for use in poor atmospheric conditions, commonly used in radar on UAVs, aircraft, marine ships, and rotorcraft, foreign object debris detection on runways, use in security check systems, and Satellite communications systems. |
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| RISC-V FT based OBC for LEO Applications | |
Satellite On-Board Computer (OBC)
from SkyLabs d.o.o.
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| The NANOhpm-obc from SkyLabs d.o.o. is a high-performance RISC-V on-board computer that is designed for most demanding LEO applications. It provides a versatile design in terms of variety of resources and available interfaces. It is built on a robust NANOobc architecture, enhanced with significantly greater processing power, delivering 100 DMIPS at 50 MHz. It delivers fault-tolerant NOEL-V processor in a peripheral-rich SoC design. |
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| 25.5-27 GHz Hemispherical Antenna Pointing Mechanism | |
Antenna Positioning Mechanism
from Airbus
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| The LEO Ka-Band from Airbus is an antenna pointing mechanism designed for hemispheric coverage in low Earth orbit communications. This has an independent 2-axis movement with full azimuth rotation and variable elevation. It uses a geared stepper motor drive and contactless rotary joints for RF signal transfer. This LEO Ka-band has a slip ring for electrical signal transmission. The unit has a mass of less than 9 kg and a moving envelope of 70 x 72 cm. |
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| 5 V Radiation Hardened Comparator | |
Space Qualified Comparator
from Honeywell Aerospace
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| The HMXCMP01 from Honeywell is a Space-Qualified Comparator that is fabricated on radiation-hardened SOI-IV SOI CMOS process. It requires an analog supply of 4.75-5.25 V and a digital supply of 5.0 V or 3.3 V IO voltage. It is rad-hardened up to 3x10^5 rad (Si) and qualified by 60Co testing per MIL-STD-883 Method 1019. It is designed for low input current, low offset voltage, and fast response time while operating over the full military temperature range. |
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| Space Vehicle Separation System | |
Separation System
from Rocket Lab
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| The 2003336B from Rocket Lab is a Separation System designed to separate space vehicles from launch vehicles. This separation system has a bolt-circle diameter of 8-24 inches and a total mass of 4.48-10.99 lb. It requires a supply voltage of 24-32 V and has an initiation time of 0.005-0.035 sec. The ALB has a storage life of 3 years and is suitable for commercial, government, private and university customers, for LEO, GEO and interplanetary orbits. |
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| S-Band Dual-CP Omni Antenna for Space Applications | |
Satellite Antenna
from PlaneWave
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| The PW2020-110 from PlaneWave is a Satellite Antenna with an operating frequency of 2025-2110 MHz and a maximum axial ratio of 3 dB. The antenna has an Omni pattern coverage with a VSWR of 2:1. It has an SMA female connector that is designed to NASA GEVS specifications. It has a mass of 100 g and measures 3.2 x 3.2 x 0.84 inches. It is ideal for space communication links and TT&C applications in harsh space environments. |
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| Three-Channel Iridium SATCOM Transceiver | |
SATCOM Transceiver
from Collins Aerospace
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| The IRT-2120 from Collins Aerospace is an Iridium-based SATCOM Transceiver that operates with a DC power of 28 V. It includes maintenance and diagnostic interfaces such as an RS-232 data port, USB maintenance jack, and RJ-11 test jack, along with support for an external configuration module and SIM reader (ICM-2100). It is an ideal solution for aircraft requiring reliable SATCOM voice and ACARS data services, supporting FANS and NextGen airspace compliance. |
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| 100 V N-Channel Power MOSFET | |
Space Qualified MOSFETs
from Infineon Technologies
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| The IRHG7110 from Infineon Technologies is a Space-Qualified N-Channel Power MOSFET that has a drain-source voltage of 100 V. It has a radiation tolerance TID of up to 100 krad with IR HiRel HEXFET technology and has a pulsed drain current of 4.0 A. It is available in a hermetically sealed ceramic enclosure measuring 19.30 x 8.12 x 8.88 mm and is ideal for switching applications such as DC to DC converters and motor control, and satellite applications. |
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| 22 Nms Flight-Proven Reaction Wheel | |
Reaction Wheel
from Bradford Space
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| The W18E from Bradford Space is a Reaction Wheel that consists of a wheel drive electronics box and a reaction wheel assembly. It requires a power bus supply voltage of 28/50 VDC and has a peak power consumption of 168 W. The assembly has a mass of 5.65 Kg and measures 258 × 181 × 143 mm. It has flown on several successful missions such as SOHO, RadarSat, Seastar, Olympus, INTEGRAL, XMM, Rosetta, Aeolus, and BepiColombo. |
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| 12U Assembly JIG | |
Assembly JIG
from NPC Spacemind
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| The TP12 from NPC SPACEMIND is an Assembly JIG with a mass of 11.2 Kg. It has a payload mass of 24 kg. This Assembly JIG consists of a test pod, a regulation plate, and assembly screws. It comes with an optional form factor reducer. It is designed to maximize accessibility, ease of integration, flexibility, and compatibility with CubeSat dimensional specifications. This modular integration is customizable based on different payloads and subsystems. |
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| Satellite Laser Communication Ground Terminal | |
Satellite Laser Communication Terminal
from General Atomics
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| The Optical Ground Terminal from General Atomics is a Satellite Laser Communication Terminal with an aperture of 70 cm. It has on-off keying of 2.5 Gbps and a power consumption of 10 W. The SDA v3.0 OCT-compliant communication terminal has a transmit fiber laser of range 1530-1565 and has adaptive optics for atmospheric turbulence mitigation. It has higher data rates and alternate coherent communication protocols with CCSDS 141-10 compatibility. |
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| 120 Nm Spacecraft Thruster | |
Spacecraft Thruster
from Moog
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| The 058E151 from Moog is a Spacecraft Thruster with a nominal thrust of 120 Nm at 6.9 bar. It has a specific impulse of 65 s. This cold gas thruster has a proof pressure of 70 bar and a burst pressure of 111.4 bar. This thruster requires a supply voltage of 22-34 Vdc and a power consumption of 1.5-10.5 W. It has a mass of 70 g and measures 19.1 x 41.0 mm. The spacecraft thruster has a life of greater than 1000000 cycles and was flown on the Spitzer Space Telescope. |
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| 4 MP RGB/Monochrome Camera for Space Asset Monitoring | |
Satellite Camera
from Infinity Avionics
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| The Lynx4MP-10 from Infinity Avionics is a 4MP RGB/Monochrome camera with a 10 mm focal length wide-angle ruggedized optical assembly. It has an onboard RAM capacity of 30 full-resolution images and a flash memory of 800 full-resolution images. It has a DC power supply of 5 V. The camera has a mass of 440 grams and measures 100 x 100 x 90 mm in dimensions. It is ideal for space-based space asset monitoring and close-proximity applications. |
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