Effect of strain isolator pad modulus on inplane strain in shuttle orbiter thermal protection system tiles
By: James Wayne Sawyer
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2141
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1983
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 45
Subjects: Reusable space vehicles; Thermal stresses
Notes: Distributed to depository libraries in microfiche

"August 1983"--Cover

Subject category 39

Includes bibliographical references