NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Standardized Modular Power Interfaces for Future Space Explorations MissionsEarlier studies show that future human explorations missions are composed of multi-vehicle assemblies with interconnected electric power systems. Some vehicles are often intended to serve as flexible multi-purpose or multi-mission platforms. This drives the need for power architectures that can be reconfigured to support this level of flexibility. Power system developmental costs can be reduced, program wide, by utilizing a common set of modular building blocks. Further, there are mission operational and logistics cost benefits of using a common set of modular spares. These benefits are the goals of the Advanced Exploration Systems (AES) Modular Power System (AMPS) project. A common set of modular blocks requires a substantial level of standardization in terms of the Electrical, Data System, and Mechanical interfaces. The AMPS project is developing a set of proposed interface standards that will provide useful guidance for modular hardware developers but not needlessly constrain technology options, or limit future growth in capability. In 2015 the AMPS project focused on standardizing the interfaces between the elements of spacecraft power distribution and energy storage. The development of the modular power standard starts with establishing mission assumptions and ground rules to define design application space. The standards are defined in terms of AMPS objectives including Commonality, Reliability-Availability, Flexibility-Configurability and Supportability-Reusability. The proposed standards are aimed at assembly and sub-assembly level building blocks. AMPS plans to adopt existing standards for spacecraft command and data, software, network interfaces, and electrical power interfaces where applicable. Other standards including structural encapsulation, heat transfer, and fluid transfer, are governed by launch and spacecraft environments and bound by practical limitations of weight and volume. Developing these mechanical interface standards is more difficult but an essential part of defining physical building blocks of modular power. This presentation describes the AMPS projects progress towards standardized modular power interfaces.
Document ID
20150010215
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Oeftering, Richard
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
June 9, 2015
Publication Date
May 11, 2015
Subject Category
Electronics And Electrical Engineering
Lunar And Planetary Science And Exploration
Report/Patent Number
GRC-E-DAA-TN22953
Report Number: GRC-E-DAA-TN22953
Meeting Information
Meeting: Annual Space Power Workshop
Location: Manhattan Beach, CA
Country: United States
Start Date: May 11, 2015
End Date: May 14, 2015
Sponsors: Aerospace Corp.
Funding Number(s)
WBS: WBS 756414.01.99.99.99.99.22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Spacecraft Power
Exploration
Spacecraft Architecture
No Preview Available