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Near-term Persistent Platform Orbital Testbed: Three Candidate Architecture Options On-orbit Servicing, Assembly, and Manufacturing (OSAM) will revolutionize the space industry by transforming the concept of operations of space systems and enabling new, radically different system implementations. These new implementations will benefit from a novel persistent asset design paradigm which focuses on evolvable designs that are tailored to the operational environment, not the launch environment. In addition, the ability to launch sub-systems independently enable future persistent assets to economically expand in capability and size, achieving cost effective and productive operations lasting for decades like terrestrial observatories. With few exceptions (International Space Station, Hubble Space Telescope, Mission Extension Vehicle customers), current space systems are not visited once they are operational. Leveraging emerging low cost commercial launch provides the ability to repeatedly and routinely revisit space systems. Thus, revolutionary new approaches for space system design are possible, creating completely new opportunities for small businesses and accelerating the growth of already established space industries. To usher in the revolutionary new operational paradigm, two things are needed. First, to build confidence in the technology and new paradigm, there must be a leading example, a bellwether persistent asset, that demonstrates the reliability and maturity of the new persistent asset paradigm (where repeated visits are common). Second, in order to rapidly advance and validate OSAM capabilities, an efficient means is required to conduct tests in the space environment. A persistent platform testbed satisfies both these needs. The space environment exhibits a plethora of characteristics that are difficult and costly to accurately simulate for a full system in a terrestrial laboratory, such as near zero gravity, a wide range of ionizing radiation types, atomic oxygen, and micro-meteoroids and space debris traveling at high velocity. In addition, since persistent assets range in mass from a few grams to several metric tons, it is difficult to accurately simulate interactions between these systems and visiting vehicles (that also exhibit a wide range of varying masses and capabilities). These interactions include the transmission of forces and/or exchanging mass (in the form of instruments, fuel, robotic assets, etc.). Thus, a rapid, versatile and cost efficient in-space testing capability that includes a persistent test platform and a surrounding in-space test zone is needed to mature technologies through experimentation. The testbed can provide common services, such as: power, thermal control, vibration isolation, data transmission between experiments and terrestrial experimenters, station-keeping, pointing, and robotic agents that can be leveraged by customer experiments. The onboard robotic agents can be used to provide payload handling services, such as: assembly, change out or upgrade, relocation, connecting/disconnecting utilities, inspection, repair or servicing, etc. Since the persistent platform cost will be amortized over many hosted payloads, its services can eventually be offered at a price much lower than if one were to design a unique and dedicated spacecraft and mission for those few experiments.
The key to achieving an effective testbed is providing efficient cost effective access and infrastructure to a variety of commercial, academic and government customers coupled with extensibility, in the capability of an individual persistent platform test bed or replication of the test bed in a different operational regime. Three potential options for implementing a test bed were developed and evaluated in this study.
Document ID
20205008304
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Bill Doggett
(Langley Research Center Hampton, Virginia, United States)
John T Dorsey
(Langley Research Center Hampton, Virginia, United States)
Brace W. White
(Langley Research Center Hampton, Virginia, United States)
Kyongchan Song
(Langley Research Center Hampton, Virginia, United States)
Lauren M. Raffanello
(Langley Research Center Hampton, Virginia, United States)
Julia E. Cline
(Langley Research Center Hampton, Virginia, United States)
John E Teter
(Langley Research Center Hampton, Virginia, United States)
Dale C. Arney
(Langley Research Center Hampton, Virginia, United States)
John R Cooper
(Langley Research Center Hampton, Virginia, United States)
Matthew K Mahlin
(Langley Research Center Hampton, Virginia, United States)
James H. Neilan
(LARC Hampton, Virginia, United States)
Jason R. Neuhaus
(LARC Hampton, Virginia, United States)
Patrick A Cosgrove
(Langley Research Center Hampton, Virginia, United States)
Russell M Snyder
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Tammy Brown
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Bo J Naasz
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Iok M Wong
(National Institute of Aerospace Hampton, Virginia, United States)
Date Acquired
October 2, 2020
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: AIAA ASCEND Conference
Location: Virtual
Country: US
Start Date: November 16, 2020
End Date: November 18, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 954879.06.21.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Persistent Platform
Orbital Testbed
Orbital Servicing
Assembly and Manufacturing
Automated/Robotic Assembly
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