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Middeck Active Control Experiment (MACE), phase AA rationale to determine which structural experiments are sufficient to verify the design of structures employing Controlled Structures Technology was derived. A survey of proposed NASA missions was undertaken to identify candidate test articles for use in the Middeck Active Control Experiment (MACE). The survey revealed that potential test articles could be classified into one of three roles: development, demonstration, and qualification, depending on the maturity of the technology and the mission the structure must fulfill. A set of criteria was derived that allowed determination of which role a potential test article must fulfill. A review of the capabilities and limitations of the STS middeck was conducted. A reference design for the MACE test article was presented. Computing requirements for running typical closed-loop controllers was determined, and various computer configurations were studied. The various components required to manufacture the structure were identified. A management plan was established for the remainder of the program experiment development, flight and ground systems development, and integration to the carrier. Procedures for configuration control, fiscal control, and safety, reliabilty, and quality assurance were developed.
Document ID
19890015887
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Crawley, Edward F. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Deluis, Javier (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Miller, David W. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1989
Subject Category
Space Transportation
Report/Patent Number
NAS 1.26:185331
NASA-CR-185331
Accession Number
89N25258
Funding Number(s)
CONTRACT_GRANT: NAG1-915
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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