Hypervelocity impact of unstressed and stressed titanium in a Whipple configuration in support of the Orion Crew Exploration Vehicle Service Module propellant tanks /

Bibliographic Details

Corporate Authors:	NASA Glenn Research Center, Hypervelocity Impact Symposium
Other Authors:	Nahra, Henry K.
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:	NASA technical memorandum ; 216804.
Subjects:	Hypervelocity impact. Micromechanics. Residual stress. Crew Exploration Vehicle. Propellant tanks. Service modules. Fabrication. Spacecraft configurations.
Online Access:	https://purl.fdlp.gov/GPO/gpo11952