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dc.contributor.advisorCatalanello, Ralph F.
dc.contributor.authorHartman, David W.
dc.date.accessioned2015-11-24T23:54:02Z
dc.date.available2015-11-24T23:54:02Z
dc.date.issued1974-07
dc.identifier.urihttps://hdl.handle.net/11244/22404
dc.description.abstractPurpose of Study: The purpose of the study was to (1) develop a methodology and conceptual framework for the analysis of accident/failure experience and (2) to use this methodology to gather, analyze, and report the accident/failure experience of two types of rocket propulsion systems. The two systems, cryogenics and storables are currently being considered for the Space Shuttle's Tug/third stage.
dc.description.abstractFindings and Conclusions: The conclusions are divided into two parts; (1) Finings of Present Study and (2) Recommendations for Future Studies. Although their use in the Shuttle program will not resemble their present applications, the study's findings is that the storables would be a safer system because of their historical record. Specific recommendations for future studies include securing original documents for investigation, developing an activity level (or exposure risk), and expanding the study to include agencies outside NASA.
dc.formatapplication/pdf
dc.languageen_US
dc.rightsCopyright is held by the author who has granted the Oklahoma State University Library the non-exclusive right to share this material in its institutional repository. Contact Digital Library Services at lib-dls@okstate.edu or 405-744-9161 for the permission policy on the use, reproduction or distribution of this material.
dc.titleStudy of the accident/failure experience of cryogenic and storable propellent systems
osu.filenameThesis-1974R-H333s.pdf
osu.accesstypeOpen Access
dc.type.genreMaster's Report
dc.type.materialText
thesis.degree.disciplineBusiness Administration
thesis.degree.grantorOklahoma State University


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