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- W804009920 abstract "The reduction of residual unbalance in the space shuttle main engine (SSME) high pressure turbopump rotors was addressed. Elastic rotor response to unbalance and balancing requirements, multiplane and in housing balancing, and balance related rotor design considerations were assessed. Recommendations are made for near term improvement of the SSME balancing and for future study and development efforts." @default.
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- W804009920 date "1983-01-01" @default.
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- W804009920 title "Dynamic balance improvement program" @default.
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