NASA NTRS · 19790023171
Dual-fuel, dual-throat engine preliminary analysis
Abstract
A propulsion system analysis of the dual fuel, dual throat engine for launch vehicle applications was conducted. Basic dual throat engine characterization data were obtained to allow vehicle optimization studies to be conducted. A preliminary baseline engine system was defined.
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Obrien, C. J.. 1979-08-01. Dual-fuel, dual-throat engine preliminary analysis. https://ntrs.nasa.gov/citations/19790023171
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