CP400.85
AAC Clyde Space
The CP400.85 is a miniaturized, flight-proven processing platform with high computing power and low energy consumption, designed for CubeSat missions as a payload processor or general-purpose on-board computer.
Typed specifications34 values
Discloses 10 of 13 fields engineers filter by in this category (category median 5).
- Processor
- ARMv7-A datasheet p.2
- Mass
- 7 g datasheet p.2 7 g
- CPU clock
- 500 MHz datasheet p.3
- Envelope (L×W×H)
- 20 x 50 x 10 mm datasheet p.2 50 x 20 x 10 mm
- RAM
- 512 MB datasheet p.2 512 MB main memory | 512 MB
- Mass storage
- 0.5 GB datasheet p.2 0.5 GB main storage, flash memory | 64 GB min · optional, over 64 GB of bulk data on two SD-cards | 7.5 GB max · optional storage module of the same 2x5 cm footprint | 0.5 GB
- Operating system
- Linux Linux-based operating system · datasheet p.1
- Supply voltage
- 3.3 V nom. · typ. · datasheet p.2 3.1 V min | 5 V max | 3.1–5 V min 3.1 / typ 3.3 / max 5 | 3.1–5 V min. to max.
- Power consumption
- 0.55 W nominal · datasheet p.3 0.55 W Nominal1 | 1 W max · < 1000 mW peak | 1 W max · peak | 0.55 W nom. · when running a Fibonacci algorithm
- Operating temperature
- -45–85 °C operating · datasheet p.2
- Radiation tolerance (TID)
- 25 krad datasheet p.2 25 krad primary components radiation tolerant to over 25 krad (Si) (TBC)
- TRL
- 9 datasheet p.1
- Lead time
- 16 months product page
- Processor architecture
- ARM Cortex-A ARMv7-A · datasheet p.1
- Flight heritage
- The CP400 has been flying in LEO since 2018 on CubeSat missions and is at TRL 9. datasheet p.2
- Satellite class
- CubeSat flying in LEO since 2018 on CubeSat missions · datasheet p.1
- Performance
- 750 DMIPS datasheet p.2
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier10 lines, in the manufacturer's own wording
- TRL
- 9
- Lead time
- 16 Week
- Flown since
- 2018
- Processor
- ARMv7-A
- Clock frequency
- 500 MHz
- Ram
- 512 MB
- Storage
- 512 MB of flash memory
- Operating system
- Linux-based
- Mass
- 7 g
- Optional
- Companion board with up to 7.5 Gb of radiation tolerant storage and over 64 GB of bulk data storage
About
The CP400.85 is a miniaturised module offering powerful data processing and application flexibility. This flight-proven processing platform features high computing power, low energy consumption, and a general-purpose processing platform on a footprint of only 20 x 50 mm. It runs a Linux-based operating system, allowing users to execute various algorithms as distinct, uploadable applications with almost limitless flexibility. These applications can run in parallel, with the OS managing scheduling. Depending on the separately supplied carrier board, the module can function as a powerful payload processor or a general-purpose on-board computer. An optional storage module, with the same 2×5 cm footprint, allows for storing up to 7.5 Gb of data in reliable, radiation-tolerant storage, and optionally over 64 GB of bulk data on two SD-cards. The platform utilizes modified COTS components to withstand up to 25 krad of radiation. Its fast boot time ensures maximum system uptime for computing tasks, and its small form factor allows integration into systems like the iADCS400, saving space. The CP400 has been flying in LEO since 2018 on CubeSat missions.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.