File:Characterization and performance of a liguid hydrocarbon-fueled pulse detonation rocket engine (IA characterization109456152).pdf
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Summary
[edit]Characterization and performance of a liguid hydrocarbon-fueled pulse detonation rocket engine ( ) | ||
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Author |
Damphousse, Paul E. |
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Title |
Characterization and performance of a liguid hydrocarbon-fueled pulse detonation rocket engine |
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Publisher |
Monterey, California. Naval Postgraduate School |
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Description |
A liquid hydrocarbon-fueled PDRE was built and successfully tested at the Naval Postgraduate Schoolαs Rocket Propulsion and Combustion Laboratory. The first time use of a new electro-hydraulic liquid fuel injector was demonstrated to produce consistent atomization properties while allowing for varying fuel injection durations at frequencies up to 50Hz. Planar laser-induced fluorescence and high-speed imaging were used to characterize the injection flow paths of this injector. Using gaseous ethylene as a baseline for comparison, the PDRE was operated at various equivalence ratios and frequencies up to 40 Hz. Operation in partial fill scenarios was successfully conducted and found to deliver a decreased impulse linearly related to the percentage fill. A series of tests was conducted using liquid JP-10 and RP-1 fuels over varying oxidizer-to-fuel ratio. The higher pressures, wave speeds, and resulting impulse measurements revealed the benefits of using high energy density hydrocarbon fuels. The difficulty in detonating these fuels was demonstrated and overcome using a variety of different geometries and hardware configurations. Subjects: Detonation |
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Language | English | |
Publication date | December 2001 | |
Current location |
IA Collections: navalpostgraduateschoollibrary; fedlink |
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Accession number |
characterization109456152 |
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Source | ||
Permission (Reusing this file) |
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted. |
Licensing
[edit]Public domainPublic domainfalsefalse |
This work is in the public domain in the United States because it is a work prepared by an officer or employee of the United States Government as part of that person’s official duties under the terms of Title 17, Chapter 1, Section 105 of the US Code.
Note: This only applies to original works of the Federal Government and not to the work of any individual U.S. state, territory, commonwealth, county, municipality, or any other subdivision. This template also does not apply to postage stamp designs published by the United States Postal Service since 1978. (See § 313.6(C)(1) of Compendium of U.S. Copyright Office Practices). It also does not apply to certain US coins; see The US Mint Terms of Use.
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This file has been identified as being free of known restrictions under copyright law, including all related and neighboring rights. |
https://creativecommons.org/publicdomain/mark/1.0/PDMCreative Commons Public Domain Mark 1.0falsefalse
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current | 14:56, 15 July 2020 | 1,275 × 1,650, 116 pages (2.21 MB) | Fæ (talk | contribs) | FEDLINK - United States Federal Collection characterization109456152 (User talk:Fæ/IA books#Fork8) (batch 1993-2020 #11215) |
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Short title | Characterization and performance of a liguid hydrocarbon-fueled pulse detonation rocket engine |
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Author | Damphousse, Paul E. |
Software used | Damphousse, Paul E. |
Conversion program | Acrobat PDFWriter 5.0 for Windows NT |
Encrypted | no |
Page size |
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Version of PDF format | 1.4 |