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Integration and Test of Shuttle Small PayloadsRecommended approaches for space shuttle small payload integration and test (I&T) are presented. The paper is intended for consideration by developers of shuttle small payloads, including I&T managers, project managers, and system engineers. Examples and lessons learned are presented based on the extensive history of 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; (7) Postflight operations. This paper is of special interest to those payload projects that 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
20030060480
Acquisition Source
Goddard Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Wright, Michael R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
NAS 1.15:211611
NASA/TM-2003-211611
Rept-2003-00086-0
Report Number: NAS 1.15:211611
Report Number: NASA/TM-2003-211611
Report Number: Rept-2003-00086-0
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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