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Astrobee Free-Flyer Nozzle MechanismThis paper describes the development and design of the Astrobee Free-Flyer propulsion nozzle assemblies. As will be illustrated in this paper, the Free-Flyer nozzles are thrust control devices used to propel the Astrobee Free-Flyer robot autonomously inside the International Space Station (ISS). The development process, design evolution, and prototyping methods, are described. Key design features are discussed in greater detail to highlight how a seemingly simple design can present surprisingly large challenges. Several lessons learned are given.
Document ID
20200010327
Acquisition Source
Ames Research Center
Document Type
Conference Paper
External Source(s)
Authors
Earl Daley
(Ames Research Center Mountain View, California, United States)
Date Acquired
May 18, 2020
Subject Category
Mechanical Engineering
Report/Patent Number
ARC-E-DAA-TN78562
Report Number: ARC-E-DAA-TN78562
Meeting Information
Meeting: The 45th Aerospace Mechanism Symposium
Location: Houston, TX
Country: US
Start Date: May 13, 2020
End Date: May 15, 2020
Sponsors: Mechanisms Education Association
Funding Number(s)
WBS: 354108.04.22.21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
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