Creep-rupture behavior of candidate Stirling engine alloys after long-term aging at 760C in low-pressure hydrogen
By: Robert H. Titran ; [prepared for U.S. Department of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D].
Contributors: United States. Dept. of Energy. Office of Vehicle and Engine Research and Development.; United States. National Aeronautics and Space Administration.
Series: NASA TM -- 83676.; NASA technical memorandum -- 83676.
Publisher: National Aeronautics and Space Administration
Published: 1984
Place of publication: [Washington, D.C.?
Language: eng
Format: Microform
Subjects: Stirling engines -- Testing.; Iron alloys -- Analysis.
Notes: "May 1984."

"Interagency agreement DE-AI01-77CS51040."

"N84-25793"--Microfiche header.

"DOE/NASA/50140-55."

Includes bibliographical references.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1984]. 1 microfiche ; 11 x 15 cm.