Analytical modeling of pressure wall hole size and maximum tip-to-tip crack length for perforating normal and oblique orbital debris impacts
Subtitle: final report for period 01 April 1995 to 31 July 1997, contract NCC8-28
By: by William P. Schonberg and Essam Mohamed.
Contributors: Mohamed, Essam.; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- 205751.; NASA contractor report -- NASA CR-205751.
Publisher: Civil & Environmental Engineering Dept., University of Alabama in Huntsville; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1997
Place of publication: Huntsville, Ala; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Impact loads.; Crack initiation.; Crack propagation.; Hole geometry (Mechanics); Holes (Mechanics); Mathematical models.; Spacecraft modules.; Kinetic energy.; Spacecraft configurations.
Notes: Shipping list no.: 98-1014-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 3 microfiches.