| Featured Space and Satellite Products |
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| 225 W Space-Qualified L-Band Circulator | |
Space Qualified Circulator
from Smiths Interconnect
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| The L Band High Power Circulator from Smiths Interconnect is a Space Qualified Circulator with a frequency range of 1.57-1.62 GHz and has an insertion loss of 0.15 dB. It has a return loss of 23 dB and has a power handling value of 225 W. The circulator has a mass of 138 g and is designed for solid state power amplifiers (SSPA) used aboard space communication, navigation, RadarSats and satellite payloads (GEO/MEO and LEO constellations). |
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| 10-40 MHz Ultra-Miniature Precision TCXO for GPS Receivers | |
Space Qualified Oscillator
from Connor-Winfield Corporation
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| The C34 from Connor-Winfield Corporation is a Space Qualified Oscillator with a frequency range of 10-40 MHz and a frequency stability of +/- 2.0 ppm. This temperature-compensated crystal oscillator requires a DC supply voltage of 3.3 V and a supply current of 2 mA. It has a low period jitter of 3-5 ps rms and an integrated phase jitter of 0.3-1.0 ps rms. It comes in an ultra-miniature 2.5 x 3.2 mm hermetically sealed ceramic SMT package. |
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| Flight-Proven 12U Satellite Deployer | |
Satellite Deployer
from Astro-und Feinwerktechnik Adlershof GmbH
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| The PSL12U from Astro-und Feinwerktechnik Adlershof GmbH is a Space-Qualified Satellite Deployer that is designed for 12U CubeSat configurations. This flight-proven deployer features a non-explosive lock and release mechanism and a deficient power consumption mechanism. It has redundancy in the actuation and deployment confirmation signals with patented fixation of the CubeSat in X, Y, and Z during launch. It measures 340.5 x 226.3 x 226.3 mm. |
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| 640 x 512 Satellite Camera for Hyperspectral Imaging Applications | |
Satellite Camera
from Raptor Photonics
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| The Owl 640 T from Raptor Photonics is a Satellite Camera with a resolution of 640 x 512 and a pixel pitch of 10 x 10 µm. This camera has an active area of 6.4 x 5.12 mm and a spectral response of 0.6-1.7 µm. It enables simultaneous capture of bright and dark portions of a scene and is designed for integration into small OEM platforms. The camera has a frame rate of up to 60 Hz. The camera has a mass of 245 g and measures 68 x 50 x 50 mm. |
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| Compact High Gain S-Band Patch Antenna | |
Satellite Antenna
from Ecuadorian Space Agency
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| The SSA03 from Ecuadorian Space Agency is a Satellite Antenna with a center frequency range of 2000-2540 MHz and a bandwidth between 80-180 MHz. It has a gain value of 7.34 dB and has an isolation value of 21 dB. The satellite antenna has a field of view of 120 degrees aperture and is constructed using Rogers 4350 space-grade antenna material. It has a mass of 9.75 g and measures 43-45 mm x 43-45 mm, depending on the CF x 2.70 mm. |
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| 13 mN Hall Effect Thruster for Operational Satellites | |
Spacecraft Thruster
from Busek
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| The BHT-200 from Busek is a Spacecraft Thruster with a nominal thrust of 13 mN and a specific impulse of 1390 seconds. It is compatible with propellants such as Xenon and Iodine and has a discharge power of 200 W. The thruster has a demonstrated impulse of 74.88 kN-s and a predicted total impulse value of 140 kN-s. The thruster has a cathode mass value of 0.12 kg and requires a DC supply voltage of 250 V. It has a thruster mass of 0.98 Kg. |
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| Inertial Measurement Units for Small Satellite Attitude Detection | |
Inertial Measurement Unit
from Micro Aerospace Solutions
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| The MASIMU01 from Micro Aerospace Solutions is a Inertial Measurement Unit for small satellite attitude detection systems with a drift of less than 1 deg/min. It has an input voltage of 5-12 V and has a power rating of 0.6 W. The IMU is combined with sun sensors, horizon sensors and other external references with thruster systems to provide a complete small satellite attitude detection and control system (ADCS). |
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| 7L Propellant Tank for Satellites | |
Spacecraft & Satellite Propellant Tank
from Antrix Corporation Limited
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| The 7L Propellant Tank from Antrix Corporation Limited is a Spacecraft & Satellite Propellant Tank with a nominal internal volume of 7.5 L and a residual volume of 100 cc. This propellant tank has an operating pressure of 24 bar and a burst pressure of 96 bar. It has a proof pressure of 36 bar with a maximum propellant flow rate of 5 cc/s. The propellant tank is constructed using Ti-6Al-4V commercially pure titanium and SS-304L. It has a dry mass of 2 kg. |
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| Space-Qualified Thermal Strap for Cryogenics and Spacecraft | |
Space Qualified Thermal Strap
from Thermal Management Technologies
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| The TMT010-205 from Thermal Management Technologies is a Space Qualified Thermal Strap that facilitates the transfer of heat while retaining elastic connections between thermal components. It is a braided construction using copper with a braid width of 12.70 mm, length of 50.80-152.40 mm, and an end height of 2.54-4.57 mm. It is ideal for applications such as cryogenic shrouds, cryocoolers, infrared instruments, superconductors, component testing, and spacecraft. |
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| Low hysteresis Nanosatellite Magnetic Torque Rods | |
Magnetorquer
from Strasspace
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| The Nanosatellite Magnetic Torque Rod from Stras Space is a Magnetorquer with a dipole magnetic moment strength of 2.0 Am^2. This magnetorquer is compatible with Micro-D connector and operates at a temperature range of -30 °C to +80 °C. It includes a linear steel alloy core with low hysteresis and has a power consumption of 450 mW. It has a mass of 230 g and is available in an aluminium enclosure measuring 135 x 47 x 27 mm. |
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| Bi-Axis Gimbal for Antenna Pointing Mechanism | |
Gimbal
from Sierra Nevada Corporation
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| The LDC20 from Sierra Nevada Corporation is a bi-axis gimbal designed for precision pointing applications requiring smooth and open-loop performance. It provides a fine step size of 0.007° at 64-microstep resolution and supports a rotational range of ±99° on both the X- and Y-axes. It has a dielectric strength of 500 VDC and an insulation resistance of 100 MΩ. The gimbal system supports a frequency of 8.025-8.4 GHz. |
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| Software Defined Radio and DSP System for Space Missions | |
Software Defined Radio
from Rincon Research Corporation
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| The AstroSDR from Rincon Research Corporation is a software-defined radio with dual receiver and transmitter that operates at 70 MHz to 6 GHz. It consists of a receiver, transmitter, FPGA, ARM processor, data storage, and high-speed I/O. The board-support-package includes pre-built functions for interfacing to the radio, ARM processor, and eMMC storage, as well as a Vivado project to assist the user in developing their own unique applications. |
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| 23 W Cryocooler for Critical Space Missions | |
Space Cryocooler
from Northrop Grumman Corporation
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| The High-Efficiency Cryocooler (HEC) from Northrop Grumman Corporation is a Cryocooler that has a refrigeration capacity of 2 W (45 K) to 23 W (150 K). This cryocooler requires a compressor input power of up to 180 W and has a reliability of greater than 90 % with up to 10 years of on-orbit operation. The cryocooler features active vibration cancellation included in TRL9 designs and supports standard digital interfaces such as RS422 and MIL-1553. |
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| Space Qualified RF Switch for Hi-Rel Applications | |
Space Qualified RF Switch
from Teledyne Relays
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| The H-32N Series from Teledyne Relays is a Space Qualified RF Switch suitable for high-reliability space flight applications. It covers a wide frequency range with F2 (L-BAND) spanning DC-2 GHz, F4 (S-BAND) covering 2-4 GHz, F8 (C-BAND) operating from 4-8 GHz and F12 (X-BAND) extending from 8-12 GHz. The RF switch has an insertion loss of up to 0.55 dB and an isolation of up to 70 dB. It has a VSWR of 1.6:1 and an operating/release time of 10 ms. |
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| 45 V P-Channel Enhancement Mode Power MOSFET | |
Space Qualified MOSFETs
from TT Electronics
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| The BS250CSM4 from TT Electronics is a space-grade P-channel enhancement mode MOSFET designed for high-reliability applications. It has a drain-source voltage of 45 V and a continuous drain current of 0.15 A. The MOSFET supports a pulsed drain current of 0.69 A and has a gate-source voltage of ± 30 V. It features a drain–source on-state resistance of 14-28 Ω. It is available in a hermetically sealed surface mount package that measures 5.59 x 3.81 x 1.40 mm. |
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