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DIAMOND - an Architecture for Persistent Space PlatformsWe define DIAMOND, an architecture for generalized, persistent platforms in space, providing support infrastructure for multiple payloads with diverse missions, and able to accept the integration of payloads delivered to the platform after it is established in space. Such platforms would create a new space ecosystem with opportunities for much larger platforms than currently exist, for adaptation to changing technological and market conditions over long periods of time, and for tenants of the platform to launch only their unique payloads without having to carry all the equipment needed to support them. The DIAMOND architecture uses a novel “Architectural Shearing Layer” approach combining long-lived but replaceable structural and support infrastructure components with shorter-lived, higher-value service and tenant facilities. The structural aspect of the proposed architecture is a regular lattice constructed of tetrahedral cells, constructed of only a few types of simple structural components, patterned according to the cubic lattice of natural diamond crystals. The cubic lattice is arranged on larger scales to be fractal sponge, providing a disproportionately large number of surface attachment points while maintaining overall low mass of the entire structure. Generalized architectural shearing layers are also provided that permit easy separation between structural, power, thermal, propulsion/attitude control, pointing/vibration control, computing/data storage, and communication, and various operational aspects of the architecture. The combined result ensures longevity by enabling space platforms to undergo many cycles of change with little peril and at low cost, changing any part of the platform at different times and rates while leaving the remaining parts of the platform undisturbed.
Document ID
20190026805
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Breidenthal, Julian
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
George, Thomas
(SaraniaSat Inc. Los Angeles, CA, United States)
Villa, Marco
(Tyvak Nano-Satellite Systems, LLC Irvine, CA, United States)
Mosleh, Ehson
(Tyvak Nano-Satellite Systems, LLC Irvine, CA, United States)
Date Acquired
July 1, 2019
Publication Date
September 12, 2016
Subject Category
Spacecraft Design, Testing And Performance
Structural Mechanics
Report/Patent Number
JPL-CL-16-3762
Report Number: JPL-CL-16-3762
Meeting Information
Meeting: AIAA/AAS Astrodynamics Specialist Conference
Location: Long Beach, CA
Country: United States
Start Date: September 13, 2016
End Date: September 16, 2016
Sponsors: American Astronautical Society, American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Other

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