Gen 2 On-Board Computer
Featuring a state-of-the-art AMD Versal adaptive SoC, NOVI's Gen 2 AI-enabled on-board computer offers un-paralleled machine-learning performance in a power efficient cube-sat form factor.
![](https://static.wixstatic.com/media/b76bcf_da5cca7cc88140a0a4ca7e561cb89db4~mv2.png/v1/fill/w_352,h_266,al_c,q_85,usm_0.66_1.00_0.01,enc_auto/b76bcf_da5cca7cc88140a0a4ca7e561cb89db4~mv2.png)
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AMD Versal ML SoC with ARM processing cores, programmable logic, and AI-engines.
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12 TOPS of ML performance.
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Radiation hardened Vorago MCU for enhanced reliability
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Integrated GNSS receiver.
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Compact form factor (93.0 x 93.0 x 32.2 mm).
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Flexible and customizable IO options (gigabit ethernet, MIPI, JESD204B, SLVS-EC, etc.).
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Shipped with Interface Control Document, user manual, and performance test data.
Gen 1 On-Board Computer
Featuring a flight-proven AMD Zynq Ultrascale+ MPSoC main processor and NVIDIA GPU for powerful processing options, NOVI's Gen 1 OBC delivers flexible edge computing capabilities.
![MicrosoftTeams-image (29).png](https://static.wixstatic.com/media/b76bcf_51fe2cc1762b4b40ab4db1f0f9964e8f~mv2.png/v1/crop/x_432,y_409,w_2950,h_2267/fill/w_427,h_313,al_c,q_85,usm_0.66_1.00_0.01,enc_auto/MicrosoftTeams-image%20(29).png)
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AMD Zynq Ultrascale+ MPSoC with ARM processing cores and programmable logic.
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256-core NVIDIA Pascal™ GPU.
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Radiation hardened Vorago MCU for enhanced reliability
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Integrated GNSS receiver.
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Compact form factor (93.0 x 93.0 x 37.4 mm).
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Flexible and customizable IO options (gigabit ethernet, MIPI, JESD204B, SLVS-EC, etc.).
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Shipped with Interface Control Document, user manual, and performance test data.
Spacecraft Bus
NOVI's team is experienced in providing end-to-end services to get your payload in space, including, spacecraft and mission design, assembly, integration and test, environmental testing, launch integration support, regulatory filings and in-space mission operations.
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Highly integrated smart satellite buses to take advantage of on-board edge computing.
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Customized development of the optimal free-flying satellite (or hosted payload) per specific use-case, leveraging a combination of in-house and COTS sub-systems.
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Tailored CONOPS to meet unique mission needs and requirements.
![](https://static.wixstatic.com/media/b76bcf_b1610e167f7840fd8da0f423ba324432~mv2.png/v1/fill/w_60,h_31,al_c,q_85,usm_0.66_1.00_0.01,blur_2,enc_auto/b76bcf_b1610e167f7840fd8da0f423ba324432~mv2.png)