Equipment Catalogue
Space Inventor's suite of satellite equipment, covering power, communications, onboard data handling, and guidance, navigation, and control (GNC) products, offers unparalleled expandability, performance, and redundancy.
MONOPOLE2-UHF
The UHF/VHF Monopole Antenna for Satellite is a high-performance, compact antenna designed specifically for satellite communication applications in the UHF & VHF bands.
FSS-P4
Fine Sun Sensor.
The highly integrated fine sun sensor uses four photodiodes to estimate the sun direction vector with a precision of 1º (1σ). The module has a built-in microcontroller which enables connectivity to a CSP network via CAN bus and readily integrates the fine sun sensor with an attitude determination and control system.
MT-6-P4
Magnetorquer rod for momentum dumping of LEO satellites.
The MT-P4 magnetorquer rod is an integrated solution designed for momentum dumping of LEO satellites. The core is annealed Alloy 79 wound with enameled copper winding and optimized for low power consumption at nominal magnetic dipole of 6 Am2.
PDU-12V-P4
Power Distribution Unit. The PDU-P4 comes in three variants featuring three different output voltage levels all communicating via CAN protocol.
The PDU-P4 is an 8-channel power distribution unit in a rugged, compact and modular enclosure. The unit includes four output connectors, each equipped with two power lines and redundant CAN.
PDU-5V-P4
Power Distribution Unit. The PDU-P4 comes in three variants featuring three different output voltage levels all communicating via CAN protocol.
The PDU-P4 is an 8-channel power distribution unit in a rugged, compact and modular enclosure. The unit includes four output connectors, each equipped with two power lines and redundant CAN.
SDR-SS-P4
Software Defined Radio. Modular software defined radio platform for TTC and payload communication.
The radio system is designed to work with the latest CCSDS Cat A recommendations for high data rate transmissions and high spectral efficiency.
IMU-P4
Inertial Measurement Unit with integrated gyroscope, accelerometer and magnetometer for satellites.
WHL-500-P4
Reaction Wheel for microsatellites.
Space Inventor presents high-performance reaction wheel units, meticulously designed for microsatellite missions with mission lifetimes of up to 5 years. These units feature an integrated 3-phase outrunner permanent magnet synchronous motor (PMSM) equipped with fully integrated motor control electronics and software, ensuring seamless and efficient satellite attitude control.
WHL-200-P4
Reaction Wheel for microsatellites.
Space Inventor presents high-performance reaction wheel units, meticulously designed for microsatellite missions with mission lifetimes of up to 5 years. These units feature an integrated 3-phase outrunner permanent magnet synchronous motor (PMSM) equipped with fully integrated motor control electronics and software, ensuring seamless and efficient satellite attitude control.
WHL-100-P4
Reaction Wheel for microsatellites.
Space Inventor presents high-performance reaction wheel units, meticulously designed for microsatellite missions with mission lifetimes of up to 5 years. These units feature an integrated 3-phase outrunner permanent magnet synchronous motor (PMSM) equipped with fully integrated motor control electronics and software, ensuring seamless and efficient satellite attitude control.
Designed with redundancy at the core, including power distribution, CAN buses, and microcontrollers, and enhanced with selective surface anodization for optimal thermal and electrical efficiency, our modules are proven in the rigors of space, from Low Earth to Geostationary Orbits.
Space Inventor provides the key to advanced satellite functionality across all critical systems.
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