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Design, Development, Testing, and Evaluation: Human Factors EngineeringWhile human-system interaction occurs in all phases of system development and operation, this chapter on Human Factors in the DDT&E for Reliable Spacecraft Systems is restricted to the elements that involve "direct contact" with spacecraft systems. Such interactions will encompass all phases of human activity during the design, fabrication, testing, operation, and maintenance phases of the spacecraft lifespan. This section will therefore consider practices that would accommodate and promote effective, safe, reliable, and robust human interaction with spacecraft systems. By restricting this chapter to what the team terms "direct contact" with the spacecraft, "remote" factors not directly involved in the development and operation of the vehicle, such as management and organizational issues, have been purposely excluded. However, the design of vehicle elements that enable and promote ground control activities such as monitoring, feedback, correction and reversal (override) of on-board human and automation process are considered as per NPR8705.2A, Section 3.3.
Document ID
20070008229
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Adelstein, Bernard
(NASA Langley Research Center Hampton, VA, United States)
Hobbs, Alan
(NASA Langley Research Center Hampton, VA, United States)
OHara, John
(Brookhaven National Lab. Upton, NY, United States)
Null, Cynthia
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
December 1, 2006
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2006-214535
L-19317
NESC-RP-06-108/05-173-E
Report Number: NASA/TM-2006-214535
Report Number: L-19317
Report Number: NESC-RP-06-108/05-173-E
Funding Number(s)
WBS: WU 843515.02.01.07.03.01.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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