Space Inventor ApS

Manufacturer DK Verified
36 Products
11 Years Active
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About Space Inventor ApS

Space Inventor ApS was founded in 2015 in Aalborg, Denmark by a team of experienced satellite engineers aiming to accelerate the development cycle and lower the cost of small satellite missions. The company operates with full vertical integration, designing and manufacturing their own avionics, attitude control systems, and satellite platforms without relying on ITAR-controlled components, making their products accessible to an international customer base.

The company product portfolio spans modular power platforms, guidance navigation and control (GNC) suites with integrated star trackers, reaction wheels, on-board data handling systems, satellite antenna systems, and complete satellite platforms from 6U CubeSats up to 16U and BIG CAT class microsatellites. Their satellite buses have been selected for missions by governmental clients including the Austrian Ministry of Defense, which commissioned the BEACONSAT satellite to detect GNSS jamming and spoofing.

Space Inventor maintains offices in Aalborg (headquarters), Copenhagen, and Leuven (Belgium), and has established itself as a reliable supplier for both commercial and dual-use satellite applications. The company targets high reliability and long operational lifetimes as key differentiators, positioning their platforms for demanding missions requiring proven industrial-grade quality.

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Products

36

Modular 12U CubeSat with electric propulsion and reaction wheels for high manoeuvrability and precise attitude control.

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16U Bring-Into-Use (BIU) CubeSat designed for direct injection into geostationary orbit using Ka, Ku and other bands.

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16U CubeSat equipped with a 200mm hyperspectral telescope for scientific and environmental observation missions.

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High-performing 16U CubeSat platform with GEO options and flight heritage in both GEO and LEO.

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6U maritime AIS/VDES satellite with a 3-element crossed deployable yagi antenna for maritime communication and navigation.

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Dependable 6U CubeSat platform for secure and tactical communication with a 10-year mission life.

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High-performing 6U satellite for secure, tactical communication between space and Earth with a 10-year mission life.

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High-performance 8U CubeSat with reaction wheels, star tracker and dual redundant buses for demanding missions.

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Microsatellite configured as an astro observatory with a 300 mm aperture telescope suitable for a range of cameras.

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Lithium-Ion satellite battery module, 8-cell 28.8V nominal, 100 Wh capacity, with daisy-chain expansion.

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ESPA-class microsatellite platform (up to 100 kg) built from flight-proven, in-house modules for a quarter-plate payload adapter.

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ESPA-class microsatellite platform (up to 300 kg) with half-plate payload adaptor for high-demand missions.

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ESPA Grande-class microsatellite platform (up to 600 kg) with full-plate payload adapter for heavy-duty missions.

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Microsatellite platform configured for Electronic Support Measures (ESM) missions with hi-reliability, shielded subsystems.

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Highly integrated fine sun sensor using four photodiodes for sun direction estimation with sub-degree precision.

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Small ESPA-class geostationary communications microsatellite engineered for LEO or GTO launch with onboard propulsion for orbit raising.

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Complete, scalable Guidance, Navigation and Control system combining sensors, actuators and control software for CubeSats and MicroSats.

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Fully-integrated, flight-proven GNC suite with star tracker and integrated ADCS for CubeSats and microsatellites.

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Compact, rugged inertial measurement unit with redundant gyroscopes, accelerometers and magnetometers.

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Compact single-port L-band patch antenna for GPS, satellite communication and remote sensing applications.

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Magnetorquer rod for momentum dumping of LEO satellites, with redundant windings and driver electronics.

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Scalable power architecture built on P4-series equipment, supporting solar array power from a few hundred watts up to 4 kW.

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Scalable power architecture for CubeSats and small satellites, providing modular EPS solution with flexible configuration.

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Scalable power architecture for CubeSats and small satellites, providing modular EPS solution with flexible configuration.

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4-channel maximum power point tracker battery charger connecting solar panels to the spacecraft battery bus.

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Quad-core ARM Cortex-M7 onboard computing platform for redundant mission-critical satellite functions.

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Redundant power distribution unit with 8 protected output channels and multiple regulated voltage variants.

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High-performance reaction wheel for microsatellite attitude control, available in 500 and 1000 Nms configurations.

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Compact single-port S-band 2x2 patch antenna array offering improved gain and reliability.

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Compact single-port S-band patch antenna for satellite communication and radar applications.

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Software-defined radio with dual full-duplex S-band or S/X-band channels and 64 GB of persistent storage.

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Microsatellite configured for real-time tracking, detection and characterization of space objects for collision avoidance and SSA.

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Ultra-low microvibration reaction wheels for precise attitude control of small satellites.

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Star tracker unit for mini- and microsatellites, based on Space Inventor's advanced star-tracking algorithms.

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High-frequency single-port X-band 4x4 antenna array for radar, satellite communication and defence applications.

1 3

Versatile payload and onboard computing platform based on a dual-core ARM Cortex-A9 SoC with integrated FPGA logic.

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