Summary
The NanoAvionics Multi-purpose Redundant 16U Bus (MP16-R) is designed for space applications. It consists of a flight computer, payload controller, electric power system, communication, and propulsion systems. Its propulsion unit also provides satellites with decommissioning capability at the end of the mission. The MP16-R satellite bus is optimized for IoT, M2M, ADS-B, AIS, commercial and emergency communication applications as well as scientific missions.
Key features
- Total Empty Bus Mass: 8000 / 9000 g
- Payload Volume: up to 12 U
- M16P Bus is already pre-integrated (mechanically, electrically and functionally tested) and pre-qualified to be ready for instant payload integration. Therefore, final flight acceptance and flight readiness procedures are minimized for the Customer.
- Default operation of M16P Bus during satellite mission is implemented at command level by execution of uploaded scripts.
- A sophisticated mission code can be prepared by the NanoAvionics team according to separately agreed terms and conditions.
- A payload integration service can be performed by the NanoAvionics team according to separately agreed terms and conditions.
- Inter-satellite link for regular connectivity.
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Last updated: 2023-03-08
Multi-purpose Redundant 16U Bus (MP16-R)
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