NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
C-SiC Composite Structures for Active CoolingThis viewgraph presentation provides an overview of research being conducted on the use of C-SiC composite structures for actively cooling rocket nozzles. Potential payoffs and design constraints are discussed. Other topics covered include: testing parameters, material selection, thermal analysis of joined tube structure, pressure containment, H2O2 combustion testing, and cooled re-entry.
Document ID
20030064976
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Marshall, D. B. (Rockwell Scientific Co., LLC Thousand Oaks, CA, United States)
Cox, B. N. (Rockwell Scientific Co., LLC Thousand Oaks, CA, United States)
Berbon, M. Z. (Rockwell Scientific Co., LLC Thousand Oaks, CA, United States)
Porter, J. R. (Rockwell Scientific Co., LLC Thousand Oaks, CA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Composite Materials
Meeting Information
Meeting: 27th Annual Conference on Ceramic, Metal and Carbon Composites
Location: Cocoa Beach, FL
Country: United States
Start Date: January 27, 2003
End Date: January 30, 2003
Funding Number(s)
CONTRACT_GRANT: NAS8-00141
Distribution Limits
Public
Copyright
Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available