Imagine a miniature telescope the size of a shoebox that can zoom in on distant stars to see if they are too volatile for life to exist. Instead of spending decades and billions on a giant observatory, this project builds a small, agile satellite that does the job quickly. It's like switching from a massive city bus to a fleet of nimble delivery scooters to get data faster.
Traditional space science satellites are too expensive and take too long to build, creating a bottleneck for astronomical data collection.
A 16U CubeSat ready for launch, featuring an Intelligent Payload Controller (IPC) and a high-performance pointing system (ADCS).
If you are a component manufacturer dealing with slow development cycles for scientific payloads — this project developed an Intelligent Payload Controller (IPC) that provides an advanced interface between the platform and the payload. This allows for faster integration and a radically faster pace of delivery.
If you are a data provider dealing with the high cost of traditional space observatories — this project developed a 16U configuration that delivers high-performance pointing accuracy. This proves that low-cost satellites can provide data complementary to the James Webb Space Telescope.
If you are a sensor developer dealing with thermal management in vacuum environments — this project developed a specific thermal design for UV spectroscopy. This enables the observation of hundreds of stars without the need for expensive cryogenic detectors.
Based on available project data, the project demonstrates the capability to deliver satellites at lower costs than traditional science satellites, though specific unit prices are not listed.
The project specifically proves a 16U configuration, showing that small-scale CubeSats can meet high-performance science needs previously reserved for larger missions.
Based on available project data, the technology is developed by a consortium of SMEs including C3S, but specific licensing terms are not provided.
The project aims to build a ready-to-launch satellite on a rapid timescale, moving from TRL3 to TRL6 within the project period of 2022 to 2025.
The platform subsystems use heritage from the ESA funded RADCUBE mission and include a new Intelligent Payload Controller (IPC) for advanced interfacing.
The project is heavily industry-driven with an 80% industry ratio, consisting of 4 industrial partners and only 1 university. The presence of 3 SMEs suggests a lean, agile development structure focused on commercial viability and rapid prototyping rather than purely academic research.
Contact C3S ELEKTRONIKAI FEJLESZTO KFT in Hungary for technical specifications on the IPC module.
Contact us to find partners for low-cost UV satellite deployment.
