| Featured Space and Satellite Products |
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| Coaxial High-Gain Pyramidal Horn Antenna | |
Satellite Antenna
from Scientific Microwave Corporation
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| The WR28 from Scientific Microwave Corporation is a Coaxial High-Gain Pyramidal Horn Antenna that operates from 26.5-40 GHz. It delivers an antenna gain of 17-20 dB and a half-power beamwidth (HPBW) of 20° (E/H-Plane). It features excellent performance in terms of gain, bandwidth, and radiation pattern. This antenna has a side-lobe level (SLL) of less than -12 dB and a VSWR value of 1.40:1. It has an aluminum enclosure with an SMA female connector. |
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| Dual Channel DVB-S2 X-Band Transmitter for LEO Spacecraft | |
Space Transmitter
from Dragonfly Aerospace
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| The HDRTx-1.5 from Dragonfly Aerospace is a high-performance, high-data-rate X-band transmitter designed specifically for low Earth orbit micro and mini-satellites. Leveraging flight-proven technology and advanced DVB-S2 encoding, the HDRTx-1.5 optimizes link margin and maximizes data throughput with dynamic modulation capabilities. This dual-channel powerhouse delivers up to 150 Msps per channel in dual mode. |
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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 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. |
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| GNSS Receiver Module for Accurate Muzzle Velocity Testing | |
GNSS Receiver
from ReliaSat
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| The W-x8RX-RA-9296 from ReliaSat is a GNSS Receiver with an RF frequency range of 92-96 GHz and an IF frequency range of 2-6 GHz. This receiver has an LO frequency of 10.80–11.40 GHz and has an image rejection of 20 dB. It has a separate power board providing additional ESD protection with low frequency inputs, WR10 connections, single rail power supplies, and requires an input voltage of 5 V. It has a mass of 90 g and measures 28 x 57 x 24 mm. |
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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. The RGB/Monochrome camera has a pixel resolution of 2048 x 2048 and supports UART, RS485, USB2, and Ethernet data interfaces. The camera has a spatial resolution of 5 m at a 500 km orbit. It has a DC power supply of 5 V and a power consumption of 2.75 W. It has a mass of 440 grams and measures 100 x 100 x 90 mm. |
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| 9 m Ka-Band Earth Station Antenna for Communication Networks | |
Earth Station Antenna
from Norsat
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| The ESEC900KA2A from Norsat is an Earth Station Antenna with an Rx frequency range of 17.70–21.20 GHz and a Tx frequency range of 27.50–31.00 GHz. This Ka-band antenna has an Rx gain of 63.19 dBi and a Tx gain of 66.86 dBi. It has a motorized 2-axis Cassegrain design that supports circular polarization with excellent axial ratio performance of less than 1.5 dB and a reflector diameter of 9 m. It has a transmit/receive VSWR value of 1.35:1. |
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| 27.5-31 GHz Ka-Band Block-Up Converter for SATCOM Applications | |
Block Upconverter
from ERZIA
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| 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. |
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| 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 | | | |
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| Non-Pyrotechnic Space Vehicle Separation System | |
Separation System
from Rocket Lab
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| 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. |
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| Space Qualified Power Transformer | |
Space Qualified Power Transformer
from Data Device Corporation
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| The HLP-6009 from Data Device Corporation is a Space Qualified Power Transformer with a primary voltage of 1-3 V and a secondary voltage of 4-8 V. It has a pulse width of 2 μs and a DC resistance of 3 - 3.5 ohms. It is built and tested to MIL-PRF-21038, MIL-STD-883, and MIL-STD-202 standards. This transformer is gold-plated over nickel-plated Kovar leads and conveniently accommodates printed circuit board mounting. |
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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 and a form factor of 12U. 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 and measures 267.3 x 266.7 x 386.5 mm. |
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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. This reaction wheel unit has a momentum storage of 22 Nms and a maximum operational speed of 4000 RPM. 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. |
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| Multi-Band Tactical Deployable Earth Terminal | |
Satellite Terminal
from Gilat Satellite Networks
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| The DKET 3400 Series Ku-Band from Gilat DataPath is a Multi-Band Tactical Deployable Earth Terminal that operates over a Ku-band uplink frequency range of 13.75–14.50 GHz and a downlink range of 10.7–12.75 GHz. It supports customer-specified 4RU expandable modems and offers up to 54 RU rack space. It is ideal for secure, high-capacity, and rapidly deployable satellite communications for military and commercial missions. |
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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 and a continuous drain current of up to 1.0 A. 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. The MOSFET has a diode forward voltage of 1.2 V. The MOSFET is available in a hermetically sealed ceramic enclosure measuring 19.30 x 8.12 x 8.88 mm. |
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| 29-31 GHz Block Upconverter | |
Block Upconverter
from Norsat
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| The ELMTBKA016 from Norsat is a Block Upconverter with a transmit frequency range of 29.0-30.0 GHz (Commercial) and 30.0-31.0 GHz (Military). It has a gain flatness of less than 4.0 dB p-p (full band) and a saturated output power of 42 dBm. The BUC has a maximum phase noise of up to -103 dBc/Hz at 1 MHz. The unit requires an input voltage of 28–72 V DC and has a power consumption of 18 W. It weighs 1.5 kg and measures 168 x 108 x 78 mm. |
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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 and is certified for use in high-altitude environments up to 55,000 ft. This three-channel airborne transceiver is designed to deliver secure global voice and data communications along with a dedicated Short Burst Data (SBD) modem. This transceiver has a mass of 3.1 kg and measures 15.68 x 2.25 x 7.6 inches. |
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| 0.7-1 GHz Ceramic Balun for Cellular Applications | |
Space Qualified RF Balun
from Mini Circuits
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| The NCS4-102+ from Mini Circuits is a Space Qualified RF Balun with a wideband frequency range of 700-1000 MHz. This ceramic balun has an amplitude unbalance of 0.5 dB and a low phase unbalance of 5 degrees. It has an impedance ratio of 4 and a maximum insertion loss of 1.3 dB. The balun has an impedance value of 50 Ohms and a maximum RF power rating of up to 2 W. This RoHS-compliant balun has a mass of 0.008 g and measures 0.079 x 0.049 x 0.033 inches. |
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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. It has an antenna gain value of 4-5 dBic and has a dual circular polarization of both RHCP/LHCP. 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. The S-band antenna has a mass of 100 g and measures 3.2 x 3.2 x 0.84 inches. |
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| 0.1 N Spacecraft Thruster for CubeSats and Nanosatellites | |
Spacecraft Thruster
from Micro Aerospace Solutions
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| The M010HP from Micro Aerospace Solutions is a Spacecraft Thruster with a thrust value of 0.1 N and a specific impulse of 110 s. It has an inlet pressure of 350 kPa and a pulse life of more than 500,000. The thruster is developed using monopropellants like hydrogen peroxide, hydrazine, tridyne gas, and cold gas. It has a gel-propellant design for a microspacecraft propulsion module. This thruster has a mass of 11 g and has an exit diameter of 5 mm. |
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| Integrated EPS/OBC Bus Module for CubeSats | |
Satellite On-Board Computer (OBC)
from Aphelion Orbitals
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| The Integrated EPS/OBC Bus Module from Aphelion Orbitals is a Satellite On-Board Computer that has a high-performance ARM Cortex-M4 processor running PerihelionOS with development libraries. This module supports five maximum power point tracking (MPPT) inputs with up to 40 W input capacity and delivers power through seven independently controlled and monitored output voltages of 3.3-5 V. |
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| Modular Electrical Power System for CubeSat Missions | |
Satellite Electrical Power System
from ISISPACE
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| The IMEPS2 from ISISPACE is a Satellite Electrical Power System designed for CubeSat missions from 3U upwards. This second-generation EPS has multiple configurations with an energy storage capacity of 45-135 Wh. The power system communicates over dual I²C or UART interfaces (with optional SPI), FRAM-based MCUs, rich telemetry, and GaN-FET solar interfaces for high efficiency. It is ideal for larger nano- and micro-satellites. |
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