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Dual-fuel, dual-throat engine preliminary analysis

NASA NTRS · Contractor Report (CR) · 19790023171 · Published 2019-06-21 · Legacy CDMS · 1 author

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Abstract and citation only, verbatim from NASA NTRS; full text lives there. All credit to the authors and Legacy CDMS.

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.

Author

  • Obrien, C. J. Aerojet Liquid Rocket Co.

Citation

Obrien, C. J. (2019). Dual-fuel, dual-throat engine preliminary analysis. Legacy CDMS. NASA NTRS ID 19790023171. https://ntrs.nasa.gov/citations/19790023171 ↗