Space

3-5m GSD resolution optical Earth observation satellite, based on our smaller, non-redundant, cost-efficient HyperSat platform.

1-2m GSD resolution optical Earth Observation capabilities, based on our redundant microsatellite HyperSat platform.

Synthetic Aperture Radar (SAR) Earth Observation capabilities with a resolution of up to 3-5m GSD.

With a dry mass of approximately 30 kg (including payload), Kestrel offers capabilities comparable to established 16U CubeSat platforms while featuring a payload bay more than twice as large. Its versatility allows it to support various mission profiles, including IOD, Earth observation, communications, and more.

With a dry mass of up to 100 kg (including payload), Eagle can accommodate advanced, power-intensive instrumentation for Earth observation, communications, technology, security, science, space logistics, and other mission types. Its full redundancy ensures reliable operation over an extended period.

Need a dedicated spacecraft? HyperSat’s modular architecture allows us to design a space system tailored to your needs, using subsystems with flight heritage. Contact us for more information.

Our Inception workshops provide a mission concept, plan, and preliminary cost structure, empowering our clients to take the next steps in their space journey with a detailed mission blueprint designed to ensure success and minimize risks.

We support our clients at every stage of their journey into space. Leveraging our experience, we also offer satellite registration, insurance, and launch acquisition services to identify the most advantageous solution.

Our dedicated Mission Control Centre in Warsaw and its operators are ready to handle each client's mission operations, effectively translating tasks and requirements into concrete results.

We turn raw EO data into actionable insights by providing advanced Payload Data Ground Segment solutions tailored to our customers' requirements. We offer flexibility with cloud or on-premises deployment options and advanced Artificial Intelligence algorithms trained for specific use cases.

We offer assembly & integration services for satellite missions in a dedicated ISO 7 (Class 10,000) cleanroom, equipped to enable assembly and testing of individual elements of space electronics, as well as integration of satellites weighing up to 150 kg.

Various electronic subsystems produced at Creotech Instruments have already been successfully flight-validated. TRL: 9 (flight proven)

We can manufacture main and/or auxiliary harnesses to ESA standards. Several harnesses produced at Creotech Instruments have already been successfully flight-validated. TRL: 9 (flight proven)

We offer design and manufacturing services for custom solar panels with the following features: structure mounted or deployable, high efficiency triple junction cells, up to 80W per panel, reverse bias protection, configurable cells connection – multiple cells in series or parallel, high radiation resistance, atomic oxygen resistance, temperature sensor can be added on demand. Current TRL: 6 (full-scale demonstration in relevant environment)

We offer a scalable battery management module with the following features: 80Wh capacity with 8S1P configuration; 3-5 year lifetime depending on depth of discharge and battery cycles; included battery charge controller and balancer; overcurrent, overvoltage, undervoltage, under discharge protection; RS-485 interface; unregulated 28V nominal voltage; stackable battery packs. Current TRL: 6 (full-scale demonstration in relevant environment). The picture shows a prototype.

We offer a scalable electrical power subsystem with the following features: configurable number of MPPT modules, capable of operating with our solar panels, power conditioning and distribution unit in the form of SpaceVPX module, single strain or fully redundant system, up to 200W power throughput, unregulated 28V, regulated 12V and 3.3V outputs, included LCL protection, compatibility with electric propulsion systems. Current TRL: 6 (full-scale demonstration in relevant environment)

We offer design and manufacturing services for thermal control systems: we assist to select best TCS solutions: heat pipes, heaters, radiators, experience with several coating solutions: paint, anodizing, MLI, assistance in thermal vacuum testing,. Current TRL: 6 (full-scale demonstration in relevant environment)

We offer full support in design and assembly of Multi-Layer Insulation for space missions: up to 16 grounded layers, assembly with adhesives, velcro attachment to the spacecraft. Current TRL: 9 (flight proven)

We offer an onboard computer subsystem with the following features: spaceVPX 3U form factor, multiple SpaceWire interfaces, ARM microcontroller with 100Mhz clock, 128MB operational memory, 64GB for data storage, 8MB non-volatile FeRAM memory for application image, software port of RTEMS operating system with board support package and drivers, current. TRL: 6 (full-scale demonstration in relevant environment)

We offer a CCSDS engine with the following features: spaceVPX 3U form factor; spaceWire, LVDS, RS485 interfaces for communication with bus and radio modules; fully compliant with CCSDS communication standard; data encryption and authentication; up to 50Mbit throughput. Current TRL: 9 (flight proven)

We offer full support in the design and manufacture of spacecraft harnesses for space missions: support in harness design for fully space qualified or COTS based projects; harness design for high power/ high throughput/ low level signals (shielded). Custom harness configuration possible, experience with internal/external harness (atomic oxygen resistance etc.), compliance with industry standards (ESA/NASA/custom tailoring). Current TRL: 6 (full-scale demonstration in relevant environment)

For each our subsystem we offer an electrical ground support equipment for testing and integration. We can also provide EGSE for custom subsystems with following capabilities: EGSE testers/ subsystem simulators; spaceWire, LVDS, RS422/485, UART, I2C, CANbus and custom interfaces possible; analog signals (sensors, power, load simulators); flexible architecture based on our Sinara products; python API. Current TRL: 8 (flight qualified)