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dc.contributor.authorGatcombe, Ernest K.
dc.contributor.authorProwell, Roy W.
dc.date.accessioned2016-02-24T19:32:16Z
dc.date.available2016-02-24T19:32:16Z
dc.date.issued1960-08
dc.identifier.citationContributed by the Machine Design Division and presented at the Annual Meeting, Atlantic City, N.J. November 29-December 4, 1959, of THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS, Paper no. 59--A-256,Transactions of the ASME, Journal of Engineering for Industry, August 1960, pp. 223-229.en_US
dc.identifier.urihttp://hdl.handle.net/10945/48015
dc.description.abstractIn this paper a rocket motor turbine-pump reduction gear system is analyzed in regard to Hertzian gear tooth contact stresses and times of contact. It is found that the Hertzian contact stresses vary from approximately 100,000 psi to 200,000 psi. The times of contact vary from three to eight viicrosec. Some observations regarding the correlation between contact times and gear failures are made. It is indicated that it may be possible to establish design limitations on the contact times to insure satisfactory gear operation. Sample calculations for evaluating each of the typical quantities found in the tables are included.en_US
dc.description.sponsorshipSponsored in part by ONRen_US
dc.publisherASMEen_US
dc.titleRocket motor gear tooth analysis (Hertzian contract stresses and times)en_US
dc.typeArticleen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)en_US
dc.contributor.departmentMechanical Engineeringen_US


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