Development of a monopropellant micro-nozzle in low temperature CO-fired ceramic tape

D. G. Plumlee; J. Steciak; A. J. Moll

Development of a monopropellant micro-nozzle in low temperature CO-fired ceramic tape

D. G. Plumlee
, J. Steciak
, A. J. Moll

Micron School of Materials Science and Engineering

University of Idaho

Research output: Contribution to conference › Paper › peer-review

Abstract

A micro-propulsion device was developed using Low Temperature Co-Fired Ceramics (LTCC). The device was powered using H₂O₂ as a mono-propellant with plans for other propellants including H₂ or propane. High concentrations of High Test Peroxide (∼ 90%) generated an adiabatic decomposition temperature of 1029 K when exposed to a silver catalyst. This decomposition reaction generated a high-energy exhaust composed of water vapor and oxygen. The LTCC micro-propulsion device was constructed by stacking cross-sectional layers to create internal three-dimensional features. Low temperature co-fired ceramics fabrication process, a mono-propellant micro-propulsion device was developed. This is an abstract of a paper presented at the 30th International Symposium on combustion (Chicago, IL 7/25-30/2004).

Original language	English
Pages	372
Number of pages	1
State	Published - 2004
Event	30th International Symposium on Combustion, Abstracts of Works-in-Progress Poster Presentations - Chicago, IL, United States Duration: 25 Jul 2004 → 30 Jul 2004

Conference

Conference	30th International Symposium on Combustion, Abstracts of Works-in-Progress Poster Presentations
Country/Territory	United States
City	Chicago, IL
Period	25/07/04 → 30/07/04

Cite this

@conference{b3f97f99038b40b4b26547aea8b629bd,

title = "Development of a monopropellant micro-nozzle in low temperature CO-fired ceramic tape",

abstract = "A micro-propulsion device was developed using Low Temperature Co-Fired Ceramics (LTCC). The device was powered using H2O2 as a mono-propellant with plans for other propellants including H2 or propane. High concentrations of High Test Peroxide (∼ 90\%) generated an adiabatic decomposition temperature of 1029 K when exposed to a silver catalyst. This decomposition reaction generated a high-energy exhaust composed of water vapor and oxygen. The LTCC micro-propulsion device was constructed by stacking cross-sectional layers to create internal three-dimensional features. Low temperature co-fired ceramics fabrication process, a mono-propellant micro-propulsion device was developed. This is an abstract of a paper presented at the 30th International Symposium on combustion (Chicago, IL 7/25-30/2004).",

author = "Plumlee, \{D. G.\} and J. Steciak and Moll, \{A. J.\}",

year = "2004",

language = "English",

pages = "372",

note = "30th International Symposium on Combustion, Abstracts of Works-in-Progress Poster Presentations ; Conference date: 25-07-2004 Through 30-07-2004",

}

TY - CONF

T1 - Development of a monopropellant micro-nozzle in low temperature CO-fired ceramic tape

AU - Plumlee, D. G.

AU - Steciak, J.

AU - Moll, A. J.

PY - 2004

Y1 - 2004

N2 - A micro-propulsion device was developed using Low Temperature Co-Fired Ceramics (LTCC). The device was powered using H2O2 as a mono-propellant with plans for other propellants including H2 or propane. High concentrations of High Test Peroxide (∼ 90%) generated an adiabatic decomposition temperature of 1029 K when exposed to a silver catalyst. This decomposition reaction generated a high-energy exhaust composed of water vapor and oxygen. The LTCC micro-propulsion device was constructed by stacking cross-sectional layers to create internal three-dimensional features. Low temperature co-fired ceramics fabrication process, a mono-propellant micro-propulsion device was developed. This is an abstract of a paper presented at the 30th International Symposium on combustion (Chicago, IL 7/25-30/2004).

AB - A micro-propulsion device was developed using Low Temperature Co-Fired Ceramics (LTCC). The device was powered using H2O2 as a mono-propellant with plans for other propellants including H2 or propane. High concentrations of High Test Peroxide (∼ 90%) generated an adiabatic decomposition temperature of 1029 K when exposed to a silver catalyst. This decomposition reaction generated a high-energy exhaust composed of water vapor and oxygen. The LTCC micro-propulsion device was constructed by stacking cross-sectional layers to create internal three-dimensional features. Low temperature co-fired ceramics fabrication process, a mono-propellant micro-propulsion device was developed. This is an abstract of a paper presented at the 30th International Symposium on combustion (Chicago, IL 7/25-30/2004).

UR - https://www.scopus.com/pages/publications/10644282238

M3 - Paper

AN - SCOPUS:10644282238

SP - 372

T2 - 30th International Symposium on Combustion, Abstracts of Works-in-Progress Poster Presentations

Y2 - 25 July 2004 through 30 July 2004

ER -

Development of a monopropellant micro-nozzle in low temperature CO-fired ceramic tape

Abstract

Conference

Other files and links

Fingerprint

Cite this