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NASA NTRS · Contractor Report (CR)

Dual-fuel, dual-throat engine preliminary analysis

Published 2019-06-21 From Legacy CDMS 1 author
Read paper (PDF) ↗ View on NASA NTRS ↗

Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

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 ↗