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.
Z7000-P4
Versatile Payload and Onboard Computing Platform.
The Z7000 is a suitable choice as a payload computer with requirements for high data-rates and processing capabilities.
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.
IMU-P4
Inertial Measurement Unit with integrated gyroscope, accelerometer and magnetometer for satellites.
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.
WHL-1000-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-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.
PDU-BAT-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.
OBC-P4
On-Board Computer. Two Cortex M7 On-Board Computers with Dual Redundancy.
The OBC-P4 is an onboard computing platform consisting of four independent ARM Cortex-M7 modules, each with separate power supply, interfacing, and storage. The dual architecture makes the OBC-P4 a suitable choice for hot/cold redundancy solutions often desired for mission critical subsystems, such as T&C, GNC, or management of valuable payloads.
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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