| Featured Space and Satellite Products |
|
|
| 30000 Ohms GSFC Space Qualified Thermistor | |
Space Qualified Temperature Sensor
from TE Connectivity
|
| The 44910 from TE Connectivity is a Space-Qualified Temperature Sensor with a resistance of 30,000 ohms and a tolerance of ±0.1 °C (0°C to 70°C). It has a beta value of 3943 K and a beta tolerance of 0.4 %. This flight-proven temperature sensor has a dissipation constant of 1 mW/°C and an insulation resistance of 500 V. It consists of a pressed disk ceramic sensor and thermally conductive epoxy coating that meet outgassing requirements. |
| |
Download Datasheet
Product Details | |
|
|
|
| 25.5-27 GHz Hemispherical Antenna Pointing Mechanism | |
Antenna Positioning Mechanism
from Airbus
|
| The LEO Ka-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 0.3° and a rotational velocity under 10°/s. It has a frequency range of 25.5–27 GHz and delivers a high antenna gain of 31 dBi. This has an independent 2-axis movement with full azimuth rotation and variable elevation. The unit has a mass of less than 9 kg and a moving envelope of 70 x 72 cm. |
| |
Download Datasheet
Product Details | |
|
|
|
| Non-Pyrotechnic Space Vehicle Separation System | |
Separation System
from Rocket Lab
|
| The 2000785H 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 to 38 inches and can support payloads of up to 200 Kg. It is TRL 9 qualified and is made with materials and methods consistent with Class-A space flight hardware. The separation system has a total mass of 3000 Kg and has integrated springs, switches, and connectors that streamline mission design. |
| |
Download Datasheet
Product Details | |
|
|
|
| 27.5-31 GHz Ka-Band Block-Up Converter for SATCOM Applications | |
Block Upconverter
from ERZIA
|
| The ERZ-BUC-2750-3100-43 from ERZIA is a Block Upconverter that converts an input frequency of 0.95-1.95 GHz to an output frequency of 27.5-31 GHz. It has an internal LO frequency range of 26.55-29.05 GHz and has a bandwidth of 1000 MHz. The block-up converter has an adjustable signal gain of 45-75 dBm and an output power of 40-43 dBm. It is a MIL-STD screened converter that requires a supply of 24-32 V and power consumption of 90-130 W. |
| |
Download Datasheet
Product Details | |
|
|
|
| Multi-Frequency GNSS Receivers for Space Navigation | |
GNSS Receiver
from Rakon Limited
|
| The GNSS DB from Rakon Limited is a GNSS Receiver with multi-band and multi-constellation support designed for small and nanosatellites. This receiver has a position accuracy of 1.2 m and a velocity accuracy of less than 3 cm/s RMS. It has a time accuracy of 5-20 nsec with a time to first fix of 45 sec cold start and 20 sec hot start. It requires an input DC voltage of 3.3 V. The receiver has a mass of 56 g and measures 55 x 41 x 16 mm. |
| |
Download Datasheet
Product Details | |
|
|
|
| SmallSat Payload Power and Data Handling Unit | |
Payload Data Handling System
from Berlin Space Technologies
|
| The PPDH110-1PL from Berlin Space Technologies is a Power and Data Handling Unit that is designed for small satellite payloads. It acts as the single interface unit between the bus and the payload. This power and data handling unit requires a DC input voltage of 20.5–25.2 V and supports RS-422 and LVDS payload data interfaces and an RS-422 TMTC interface. It has an output voltage in the range of 3.8-23.1 V. It has a mass of 780 g and measures 186 x 98 x 46 mm. |
| |
Download Datasheet
Product Details | |
|
|
|
| 28-118 W Solar Arrays for 6U/12U CubeSats | |
Satellite Solar Panel
from Blue Canyon Technologies
|
| The Solar Arrays 6U/12U from Blue Canyon Technologies is a Satellite Solar Panel with carbon fiber and honeycomb structures. It has an array power of 48-118 W and has a DC voltage of 17 or 34.1 V. This double/triple panel solar array pair, with GN&C for maximum performance, with release mechanisms and solar array drive assemblies (SADAs) for optimum sun-pointing operations. It has standard arrays that include 30 percent efficient cells. |
| |
Download Datasheet
Product Details | |
|
|
| Sponsored by PCB Directory | | PCB Directory Launches their Inaugural Magazine for the PCB Industry | | PCB Directory recently launched its Inaugural PCB Magazine for the PCB Industry. This magazine is packed with insightful articles, product listings, and an industry directory. The magazine is available in both print and digital versions. This achievement was made possible by the unwavering support of sponsors and contributors. Their trust and dedication have been the driving force behind this journey, and their support is highly appreciated. The team looks forward to continued growth and delivering even greater value to the PCB community. Click Here | | | |
|
|
| 4 MP Optical Imager for Nano Satellites | |
Satellite Camera
from AAC Clyde Space
|
| 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. This optical imager requires a maximum voltage supply of 5 V and has a maximum current consumption of 200 mA. It has a full frame size of 2048 x 1944 pixels and a standard lens focal length of 16, 25, 35, or 50 mm. It has a mass of 59 g and measures 29 x 29 x 70.7 mm. |
| |
Download Datasheet
Product Details | |
|
|
|
| Accelerometer for Solar Tracking/Pointing Systems | |
Space Qualified Accelerometer
from Solar MEMS
|
| 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. The sensors offer selectable fields of view of 10°, 30°, 50°, or 120°. It has a sensor with a mass of 100 g and measures Ø 80 × 27 mm. |
| |
Download Datasheet
Product Details | |
|
|
|
| 1-125 MHz Space-Qualified Oscillator for Space Applications | |
Space Qualified Oscillator
from Q-Tech Corporation
|
| The QT735LA from Q-Tech Corporation is a space-qualified oscillator with an operating frequency range of 1—125 MHz. This crystal oscillator requires a supply voltage of 3.3 V and a supply current of 5-40 mA. It has a rise/fall time of 2-200 ns and a startup time of 8 ns. The oscillator has a radiation tolerance of up to 50 kRad (Si) and has a phase noise of up to 158 dBc/Hz. This oscillator is available in a surface-mount package that measures 3.20 x 5.00 x 1.20 mm. |
| |
Download Datasheet
Product Details | |
|
|
|
| 5 V Radiation Hardened Comparator | |
Space Qualified Comparator
from Honeywell Aerospace
|
| The HMXCMP01 from Honeywell is a Space-Qualified Comparator that is fabricated on a radiation-hardened SOI-IV Silicon-On-Insulator (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. This comparator has a common voltage range of 0-5 V and an input offset voltage of +/- 24 mV. It has a propagation delay of less than 125 ns and output rise/fall times of 30 ns. It has a low power dissipation of 200 mW. |
| |
Download Datasheet
Product Details | |
|
|
|
| 17.7-20.2 GHz Ka-Band SATCOM Low Noise Amplifiers | |
SATCOM Amplifier System
from Orbital Research
|
| The WB Ka LNA from Orbital Research is a SATCOM Amplifier System with a frequency range of 17.7-20.2 GHz and a low noise temperature of 120 K. This Ka-band amplifier system has a gain of up to 55 dB and a gain flatness of ±1 dB over any 500 MHz. It has a gain stability of 0.2 dB and a ripple gain value of ±1.5 dB. The amplifier system has a P1dB value of 13 dB. This amplifier system has a mass of 250 g and measures 111.5 x 41.3 x 31.9 mm. |
| |
Download Datasheet
Product Details | |
|
|
|
| 30-31 GHz Ka-Band SATCOM On-The-Move Terminal | |
Satellite Terminal
from General Dynamics Mission Systems
|
| The M20-24M Ka MIL from General Dynamics Mission Systems is a Satellite Terminal with a transmit frequency range of 30-31 GHz and a receive frequency range of 20.20-21.20 GHz. This Ka-band satellite terminal has a G/T of 16.4 dB/K and an EIRP of 53.5 dBW at midband and P1dB. It has a beamwidth of 1.1-1.6 degrees and an axial ratio of 1-1.5 dB. The terminal has an azimuth travel of 360 degrees and an elevation travel of 0-95 degrees. |
| |
Download Datasheet
Product Details | |
|
|
|
| 5-18 GHz Analog Phase Shifter for RF Devices | |
Analog Phase Shifter
from Qorvo
|
| The CMD297P34 from Qorvo is an Analog Phase Shifter with a frequency range of 5-18 GHz and has a phase shift value of 220 degrees. It has an insertion loss of 7.3-17 dB and has an input/output return loss of 10 dB. The phase shifter has a control voltage range of 0-10 V and a phase voltage sensitivity of 22 degrees/volt. It has a reverse current value of 5 mA. This analog phase shifter has a Pb-Free RoHS Compliant 3x4 mm QFN package. |
| |
Download Datasheet
Product Details | |
|
|
| Sponsored by PCB Directory | | |
|
|
| Multi-band Software Defined Radio for Space Applications | |
Software Defined Radio
from L3Harris Technologies
|
| The C/TT-600 UHF-BAND from L3Harris is a Software Defined Radio designed to support a wide range of applications in LEO, MEO, GEO, Cislunar, and deep space. It has a Tx/Rx center frequency of 390-450 MHz with a frequency stability of +/-2 ppm. It has a Tx data rate of up to 12 Mbps and an Rx data rate of up to 10 Mbps. It consists of a base power supply and a digital processing module forming the base radio. This SDR measures 9 x 2 x 5 inches. |
| |
Download Datasheet
Product Details | |
|
|
|
| Hermetic Silicon Schottky Carbide Rectifier | |
Space Qualified Diode
from Sensitron Semiconductors
|
| The SHD687182 from Sensitron Semiconductors is a Space Qualified Diode with a peak inverse voltage of 1200 V and a maximum forward voltage drop range of 1.4-3 V. It has a maximum forward surge current of 13 A and a maximum DC output current of 2 A. The rectifier has a total capacitive change value of 15 nC and a total junction capacitance value of 11 pF. It has a maximum thermal resistance value of 8 degree C/W and a maximum power consumption of 18.7 W. |
| |
Download Datasheet
Product Details | |
|
|
|
| Optical Communications Terminal for Space Applications | |
Satellite Laser Communication Terminal
from Mynaric
|
| The CONDOR Mk3 from Mynaric is a satellite laser communication terminal with inter-satellite connectivity in low Earth orbit (LEO) for various applications. It supports full duplex, symmetrical, simultaneous transmit and receive with data rates from 313 Mbps up to 2.5 Gbps, with future capability extending to 10 Gbps. The terminal enables inter-satellite connections across distances greater than 6,500 km and uses laser communication technology. |
| |
Download Datasheet
Product Details | |
|
|
|
| Active GPS+GLONASS Patch Antenna Module for CubeSats | |
Satellite Antenna
from SkyFox Labs
|
| The piPATCH-LG/FM from SkyFox Labs is a Satellite Antenna designed to provide strong signal reception in space. It has a frequency range of 1.575 GHz for GPS L1 and 1.598-1.607 GHz for GLONASS G1. It is a RoHS-compliant model that requires a supply voltage of 2.7-5.5 V and a current consumption of 20 mA. The patch antenna has a mass of 50 g and measures 98 × 98 × 13 mm. It is ideal for limited power budget space projects and CubeSats. |
| |
Download Datasheet
Product Details | |
|
|
|
| 20.68 MPa Space-Qualified Valve for Spacecrafts | |
Spacecraft Valve
from Marotta Controls
|
| The CVM304 from Marotta Controls is a Spacecraft Valve with a pressure of up to 20.68 MPa. It has a proof pressure of 31.02 MPa and a burst pressure of 51.71 MPa. This valve incorporates a poppet with internal flow passages for minimal pressure drop. It has a wide variety of fluids: GN2, GHe, Seawater, Cryogenic H2, MMH, and N2O4. The poppet has a large L/D ratio for maximizing the poppet guide and minimizing chatter for smooth operation. |
| |
Download Datasheet
Product Details | |
|
|
|
| 260 mN Hall-Effect Electric Thruster | |
Spacecraft Thruster
from Bellatrix Aerospace
|
| The Arka 5000 from Bellatrix Aerospace is a Hall-effect thruster that delivers a thrust of 260 mN. It operates at a discharge power of 5 kW and provides a specific impulse of 2000 s. This electric propulsion system is part of Bellatrix’s Arka series, which incorporates innovative design improvements to enhance performance, operational life, cost, and weight savings to the HET, making it ideal for a plethora of mission requirements. |
| |
Download Datasheet
Product Details | |
|
