Session

Technical Poster Session 12: Systems

Location

Utah State University, Logan, UT

Abstract

SIL has leveraged our experience and previously qualified Intelli-Avionics® aerospace hardware to fill a technology gap within the CubeSat class platform. The popular open-frame CubeSat design is difficult to space qualify and provides minimal benefits when compared to traditional satellite bus systems. The OMSR CubeSat bus addresses these issues by providing a standard ruggedized CubeSat solution designed to improve functionality, reliability, and efficiency, while simultaneously reducing development time and recurring cost.

The OMSR CubeSat bus is composed of order-independent, stackable subsystem modules. Modules can be independently designed, tested, and qualified to negate redesign costs. Individual modules of the OMSR bus can be custom designed, can be populated with COTS components, or can be obtained from SIL as fully populated COTS subsystems. Modules are vertically integrated and network via an internal power and data backplane system. The OMSR bus provides many protection features and enables utilization of the latest CubeSat technology making it the ideal platform for advanced, extended life missions.

Available for download on Saturday, August 07, 2021

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Aug 7th, 12:00 AM

SmallSat Bus Supporting Cislunar Operations for Advanced DoD, NASA and Commercial Missions Chameleon Smart Bus 12U to ESPA

Utah State University, Logan, UT

SIL has leveraged our experience and previously qualified Intelli-Avionics® aerospace hardware to fill a technology gap within the CubeSat class platform. The popular open-frame CubeSat design is difficult to space qualify and provides minimal benefits when compared to traditional satellite bus systems. The OMSR CubeSat bus addresses these issues by providing a standard ruggedized CubeSat solution designed to improve functionality, reliability, and efficiency, while simultaneously reducing development time and recurring cost.

The OMSR CubeSat bus is composed of order-independent, stackable subsystem modules. Modules can be independently designed, tested, and qualified to negate redesign costs. Individual modules of the OMSR bus can be custom designed, can be populated with COTS components, or can be obtained from SIL as fully populated COTS subsystems. Modules are vertically integrated and network via an internal power and data backplane system. The OMSR bus provides many protection features and enables utilization of the latest CubeSat technology making it the ideal platform for advanced, extended life missions.