NASA-Z - A liner material for rocket combustion chambers-Reference-Cited by-同舟云学术

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NASA-Z - A liner material for rocket combustion chambers

Published:1991-06-24 Issue: Volume: Page:
ISSN:
Container-title:27th Joint Propulsion Conference
language:
Short-container-title:

Author:

NGUYENTAT THINH¹,GIBSON V.¹,HORN RONALD¹

Affiliation:

1. Aerojet, Propulsion Div., Sacramento, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-2487

Reference5 articles.

1. American Society forMetals,MetalsPark,Ohio, 1986 3. Reed-Hill,R.E."Physical Metallurgy Principles,"D.Van

2. TemperatureLCFof Ni-201 and 304L S.S."Advanccd Earth-to-OrbitPropulsionTechnology 1986,Conference Proceedings, Vol.11, pp172-204,NASA-MSFC,Huntsville, Alabama. 1 1

3. Ref. 1;Ref

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2. Friction Stir Welding of GRCop-84 for Combustion Chamber Liners;Journal of Propulsion and Power;2007-07

3. Bonding Processes;Materials Processing Handbook;2007-03-28

4. Friction Stir Welding of GR-Cop 84 for Combustion Chamber Liners;45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference;2004-04-19

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