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Static and Dynamic Friction Behavior of Candidate High Temperature Airframe Seal MaterialsThe following report describes a series of research tests to evaluate candidate high temperature materials for static to moderately dynamic hypersonic airframe seals. Pin-on-disk reciprocating sliding tests were conducted from 25 to 843 C in air and hydrogen containing inert atmospheres. Friction, both dynamic and static, was monitored and serves as the primary test measurement. In general, soft coatings lead to excessive static friction and temperature affected friction in air environments only.
Document ID
19950010490
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dellacorte, C.
(NASA Lewis Research Center Cleveland, OH, United States)
Lukaszewicz, V.
(Calspan Corp. Fairview Park, OH., United States)
Morris, D. E.
(Rockwell International Corp. Canoga Park, CA., United States)
Steinetz, B. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1994
Subject Category
Chemistry And Materials (General)
Report/Patent Number
NAS 1.15:106571
E-8774
NASA-TM-106571
Report Number: NAS 1.15:106571
Report Number: E-8774
Report Number: NASA-TM-106571
Accession Number
95N16905
Funding Number(s)
CONTRACT_GRANT: NAS3-25685
PROJECT: RTOP 505-63-1A
Distribution Limits
Public
Copyright
Public Use Permitted.
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