NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Development and Evaluation of High Temperature Gaskets for Hypersonic and Reentry ApplicationsA wide variety of flexible gasket compositions were developed and tested at high temperatures. The gasket material system has high temperature capability. GRABER sealants were very effective in sealing machined ACC-4 composite surfaces. The gasket composition do not bond strongly with the ACC-4 substrate materials. The density of gasket materials can be tailored to show appropriate compressibility.
Document ID
20080003824
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Singh, Mrityunjay (Ohio Aerospace Inst. Brook Park, OH, United States)
Shpargel, Tarah (ASRC Aerospace Corp. Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
October 1, 2007
Publication Information
Publication: 2006 NASA Seal/Secondary Air System Workshop; Volume 1
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Public Use Permitted.

Related Records

IDRelationTitle20080003817Collected Works2006 NASA Seal/Secondary Air System Workshop; Volume 120080003817Collected Works2006 NASA Seal/Secondary Air System Workshop; Volume 1
No Preview Available