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Integration and Test for Small Shuttle PayloadsRecommended approaches for shuttle small payload integration and test (I&T) are presented. The paper is intended for consideration by developers of small shuttle payloads, including I&T managers, project managers, and system engineers. Examples and lessons learned are presented based on the extensive history of the NASA's Hitchhiker project. All aspects of I&T are presented, including: (1) I&T team responsibilities, coordination, and communication; (2) Flight hardware handling practices; (3) Documentation and configuration management; (4) I&T considerations for payload development; (5) I&T at the development facility; (6) Prelaunch operations, transfer, orbiter integration, and interface testing; and (7) Postflight operations. This paper is of special interest to those payload projects which have small budgets and few resources: That is, the truly 'faster, cheaper, better' projects. All shuttle small payload developers are strongly encouraged to apply these guidelines during I&T planning and ground operations to take full advantage of today's limited resources and to help ensure mission success.
Document ID
20020015933
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Wright, Michael R.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Day, John H.
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Space Transportation And Safety
Report/Patent Number
IEEAC Paper-092
Report Number: IEEAC Paper-092
Meeting Information
Meeting: IEEE Aerospace Applications Conference
Location: Big Sky, MT
Country: United States
Start Date: March 9, 2002
End Date: March 15, 2002
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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