| Featured Space and Satellite Products |
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| Space-Qualified Rubidium Frequency Atomic Clock | |
Space Qualified Atomic Clock
from Safran Group
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| This MiniRAFS from Safran Group is a Space-Qualified Atomic Clock for LEO, MEO, and GEO with a design life of more than 20 years. It has a phase noise of -135 to -64 dBc/Hz, a return loss of 20 dB, a harmonics of less than 30 dBc and spurious of less than -80 dB. It requires a DC supply of 15.5-16.5 V and has a power dissipation of 10-15 W. It is ideal for applications such as space scientific missions, secure satellite communications, tracking and guidance control, and advanced low satellite orbit digital communications. |
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| High Force Linear Actuator for Space Applications | |
Space Actuator
from Moog
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| The Model-R from Moog is a Space Actuator with a resolution of 0.00094 inches and a stroke of 4.64 inches. This actuator has a force of 2000 lbf at 4.67 in/sec and a maximum force of 5,200 lbf. It requires a maximum current of 30 A and has a high axial stiffness of 295,000 lb/in. The actuator uses spherical ball rod ends and has a mass of 18.2 lbs. It incorporates 3-phase BLDC motors and high precision ball screw drive that provides extra fine resolution linear movement. The actuator is ideal for space applications. |
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| Ku to Ka-band Convertible Maritime VSAT Satellite Terminal | |
Satellite Terminal
from Intellian
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| The v100NX from Intellian is a Satellite Terminal designed for satellite tracking across LEO, MEO and GEO constellations. It has an elevation range of -20 to 115 degrees. The VSAT antenna system features an embedded dual modem mediator and Wi-Fi support. It has dynamic motor brakes with integrated encoders, MCU and skew assembly. It requires an AC supply voltage of 100-240 V and a maximum BUC power of up to 100 W. It has a mass of with 5.2 kg and measures 43.1 x 35.0 x 4.4 cm for antenna control unit. |
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| 0.22 to 47 µH Space Grade Tin/Lead Shielded Inductor | |
Space Qualified Inductor
from Vishay
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| The IHLP-3232DZ-5L from Vishay is a Space Qualified Inductor with an inductance range of 0.22-47 µH and an inductance tolerance of +/- 20 %. It has a heat rating current of 2.4-36 A and a DC saturation current range of 2.8-32 A. The inductor features a shielded construction with IHLP design and and Tin/lead Sn/Pb plated terminals. It is suitable for PDAs, notebooks, desktops, servers, high-current POL converters, high-current power supplies, battery powered devices, DC/DC converters in distributed systems, and FPGAs. |
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| Solar Panel for CubeSats Power Generation | |
Satellite Solar Panel
from AAC Clyde Space
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| The PHOTON-DD from AAC Clyde Space is a Satellite Solar Panel with a power generation capacity of up to 9 W. It has the standard acceptance of thermal cycling, illumination testing, deployment testing, sensor check and visual inspection. It is designed to be compatible with the AAC Clyde Space ZAPHOD structure range. It are designed to fit at the side panels of CubeSat structures, to provide optimized power generation from any side of the satellite. This solar panel is ideal for cubesat deployment mechanisms. |
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| 150 W Ka-Band Antenna Mount TWT Amplifier System | |
SATCOM Amplifier System
from Spacepath Communications
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| The STA4515P from Spacepath Communications is a SATCOM Amplifier System with a frequency range of 27.5-31.0 GHz and a bandwidth of 2500 MHz. The amplifier system has a transmit band noise power of less than -70 dBW/4 kHz. It requires a voltage supply of 200-240 V AC and has a maximum power requirement of 525 VA. It features an advanced cooling design that enables operation at +60 degrees C and in direct sunlight and supports RS485, RS232, Ethernet, SMP, and Webpage GUI interfaces. |
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| MUNICH NEW SPACE SUMMIT 2024 | | MUNICH NEW SPACE SUMMIT 2024 | | The Munich New Space Summit serves as a vital platform for the convergence of experts, researchers, industry professionals, and policymakers to engage in discussions, share insights, and explore collaborations within the realm of commercial space exploration. The event encompasses diverse facets of New Space, including satellite development and initiatives driven by private companies and entrepreneurial endeavors. Click here to learn more. | | | |
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| 19.7-20.2 GHz Space Qualified Band Pass Filter | |
Space Qualified RF Filter
from Mercury Systems
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| The E1911 from Mercury Systems is a Space Qualified RF Filter with a frequency range of 19.7-20.2 GHz and a maximum insertion loss of 2 dB. It has a maximum flatness of 0.4 dB and a flatness variation of 0.1 dB. It has a return loss value of 20 dB and a rejection range of 15-50 dB. The space-qualified filter features a cavity design and supports SMA and SMP connectors. It weighs 0.03 lbs and measures 0.51 x 0.966 x 1.5 inches. It is ideal for applications such as satellite communications and test equipment. |
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| Ejector Release Mechanism for Satellite Dispensing | |
Attach and Release Mechanism
from Ensign-Bickford Aerospace & Defense Company (EBAD)
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| The E1000 from Ensign-Bickford Aerospace & Defense Company (EBAD) is a Attach and Release Mechanism with a maximum release load of 4448 N. The mechanism requires an operating current of 2.25-6.5 A and has a resistance of 1.6 Ohms. It features a redundant firing unit and has a minimum cycle life of 50 cycles. It is suitable for applications such as solar array and instrument deployment, satellite dispensing, hinged cover release, and other space applications where an off angle deployment is desired. |
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| C-Band to L-Band Test Loop Translator | |
Test Loop Translator
from Peak Communications
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| The TLT672 from Peak Communications is a Test Loop Translator that translates an input C-band frequency of 5.850-6.725GHz to an L-band frequency of 950-1825 MHz. The test loop translator requires a power supply of 90-264 VAC. It features full alarm monitoring and an optional manual attenuator that is continuously variable from 0-30 dB. The test loop translator weighs 4.5 Kg and measures 19 × 1.75 × 15.7 inches. It is designed to take a sample of the transmit signal and convert it to a frequency at which it can be monitored or analyzed. |
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| 12 V Dual Output DC-DC Converter for Low Profile Applications | |
DC to DC Converter
from Crane Aerospace & Electronics
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| The MGH2812S from Crane Aerospace & Electronics is a DC to DC Converter with an input voltage of 12-50 V an output voltage of 14.40-15.60 V. It uses a synchronization feature that is included with the converter that allows the user to match the switching frequency of the converter to the frequency of a system clock. This converter is manufactured in a fully certified and qualified MIL-PRF-38534 facility and has an efficiency of up to 79%. It is ideal for use in programs requiring high reliability, small size, and high efficiency. |
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| Magnetorquer for Satellites Precise Pointing | |
Magnetorquer
from AAC Clyde Space
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| The MTQ800 from AAC Clyde Space is a Magnetorquer that is designed for applications that require 50-200 Kg satellites. It has a dipole moment of 15-30 Am2 with a control accuracy of up to +/-10 %. This magnetorquer has a unique boost mode that allows it to be pushed up to higher magnetic dipole moments for short-duration maneuvers. It has a mass of 489 g and measures 250 x 67 x 35 mm. This magnetorquer is ideal for precise pointing and rapid de-saturation of any reaction wheels in the satellite. |
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| L-Band NGC Beacon Receiver for Satellite Applications | |
Satellite Beacon Receiver
from Kratos Defense & Security Solutions
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| The NGC-004-02 from Kratos Defense & Security Solutions is a Satellite Beacon Receiver with a frequency range of 930-2300 MHz and a pre-detection bandwidth of 2-250 kHz. It can track a signal deviation of up to ±150 kHz at a rate up to 10 kHz/sec caused by source frequency drift or Doppler shift. It has a dynamic range of up to 110 dB and minimum C/No value of 35dB/Hz. This receuver is capable of receiving beacons from all commercial and military satellites including NATO, Skynet, DSCS, WGS, and ARSTRAT. |
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| MUNICH NEW SPACE SUMMIT 2024 | | |
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| 5.3 mH Space Grade Current Sense Transformer | |
Space Qualified Power Transformer
from Vanguard Electronics
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| The SCS202 from Vanguard Electronics is a Space Qualified Power Transformer with a primary voltage of 70 V and a primary current of 10 A. It has an inductance of 5.3 mH and a turns ratio of 1:50:50. This transformer has a dielectric withstanding voltage of 500 V AC. It is a space-grade transformer measures 0.610 x 0.610 x 0.475 inches and comes in a transfer molded package with tin-lead terminations. It has a design that meets the MIL-STD-981 space standards and is ideal for automatic placement. |
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| 2:1 Compact Redundancy Switch for Upconverters and Downconverters | |
SATCOM Redundancy Switch
from WORK Microwave
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| The RSCC-2 from WORK Microwave is a SATCOM Redundancy Switch with a frequency range of 0-40 GHz. This switch has an isolation of 50-85 dB. It has an automatic and manual switchover option and supports RS-232, RS422, RS-485, and Ethernet interfaces. It has an integrated uplink power control and has a switching speed of 100-400 mS. It requires an input AC supply of 240 V and has a maximum power consumption of 7 W. This redundancy switch is ideal for upconverter and downconverter applications. |
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| 10-40 MHz Ultra-Miniature Precision VCTCXO for GPS Receivers | |
Space Qualified Oscillator
from Connor-Winfield Corporation
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| The C22 from Connor-Winfield Corporation is a Space Qualified Oscillator with a frequency range of 10-40 MHz and a frequency stability of +/- 1 ppm. It has an integrated phase jitter of 0.3-1.0 ps rms. The oscillator has an SSB phase noise of up to -150 dBc/Hz and a start-up time of 10 ms. It produces clipped sine wave with an output voltage of 1 V peak-to-peak. This RoHS-compliant oscillator has an ultra-miniature 2.5 x 3.2 mm hermetically sealed ceramic SMT package and is ideal for use in GPS receivers. |
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| Autonomous Star Sensor for Earth Observation Satellites | |
Star Tracker
from Jena-Optronik GmbH
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| The ASTRO APS from Jena-Optronik GmbH is a Star Tracker that has an attitude random error of less than 1 arcsec (across boresight) and 8 arcsec (boresight). It can serve as a star tracker or navigation camera system for up to 18 years lifetime in GEO orbits. The star tracker requires a power supply of 28-100 V and has a nominal power consumption of 5-12 W. It utilizes advanced radiation hard CMOS Active Pixel Sensor detector technology for long-term missions on Telecom, Science and Earth Observation satellites. |
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