Development and preliminary testing of an electrolytic ignition microthruster for space propulsion

Ming Hsun Wu; Richard A. Yetter

Development and preliminary testing of an electrolytic ignition microthruster for space propulsion

Ming Hsun Wu, Richard A. Yetter

機械工程學系

研究成果: Conference contribution

摘要

A liquid monopropellant microthruster utilizing electrolysis for ignition was designed and fabricated using low temperature co-fired ceramic tape technology. The volume of the thruster combustion chamber was 0.82 mm3. The microthruster had integrated silver electrodes to enable ignition of hydroxylammonium nitrate based liquid monopropellants by electrolytic decomposition. Energy input as small as 1.9 J produced high temperature ignition, and ignition delay times as short as 224.5 ms were achieved. A thrust output of approximately 200 mN was measured with a voltage input of 45 V.

原文	English
主出版物標題	Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion"
發行者	Combustion Institute
頁面	246-249
頁數	4
ISBN（電子）	9781604239454
出版狀態	Published - 2007
事件	Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007: Chemical and Physical Processes in Combustion - Charlottesville, United States 持續時間: 2007 10月 21 → 2007 10月 24

出版系列

名字	Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion"

Other

Other	Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007: Chemical and Physical Processes in Combustion
國家/地區	United States
城市	Charlottesville
期間	07-10-21 → 07-10-24

All Science Journal Classification (ASJC) codes

一般化學工程
機械工業
物理與理論化學

其它文件與鏈接

引用此

Wu, M. H., & Yetter, R. A. (2007). Development and preliminary testing of an electrolytic ignition microthruster for space propulsion. 於 Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion" (頁 246-249). (Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion"). Combustion Institute.

Wu, Ming Hsun ; Yetter, Richard A. / Development and preliminary testing of an electrolytic ignition microthruster for space propulsion. Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion". Combustion Institute, 2007. 頁 246-249 (Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion").

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title = "Development and preliminary testing of an electrolytic ignition microthruster for space propulsion",

abstract = "A liquid monopropellant microthruster utilizing electrolysis for ignition was designed and fabricated using low temperature co-fired ceramic tape technology. The volume of the thruster combustion chamber was 0.82 mm3. The microthruster had integrated silver electrodes to enable ignition of hydroxylammonium nitrate based liquid monopropellants by electrolytic decomposition. Energy input as small as 1.9 J produced high temperature ignition, and ignition delay times as short as 224.5 ms were achieved. A thrust output of approximately 200 mN was measured with a voltage input of 45 V.",

author = "Wu, {Ming Hsun} and Yetter, {Richard A.}",

year = "2007",

language = "English",

series = "Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 {"}Chemical and Physical Processes in Combustion{"}",

publisher = "Combustion Institute",

pages = "246--249",

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note = "Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007: Chemical and Physical Processes in Combustion ; Conference date: 21-10-2007 Through 24-10-2007",

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Wu, MH & Yetter, RA 2007, Development and preliminary testing of an electrolytic ignition microthruster for space propulsion. 於 Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion". Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion", Combustion Institute, 頁 246-249, Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007: Chemical and Physical Processes in Combustion, Charlottesville, United States, 07-10-21.

Development and preliminary testing of an electrolytic ignition microthruster for space propulsion. / Wu, Ming Hsun; Yetter, Richard A.
Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion". Combustion Institute, 2007. p. 246-249 (Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion").

研究成果: Conference contribution

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AU - Wu, Ming Hsun

AU - Yetter, Richard A.

PY - 2007

Y1 - 2007

N2 - A liquid monopropellant microthruster utilizing electrolysis for ignition was designed and fabricated using low temperature co-fired ceramic tape technology. The volume of the thruster combustion chamber was 0.82 mm3. The microthruster had integrated silver electrodes to enable ignition of hydroxylammonium nitrate based liquid monopropellants by electrolytic decomposition. Energy input as small as 1.9 J produced high temperature ignition, and ignition delay times as short as 224.5 ms were achieved. A thrust output of approximately 200 mN was measured with a voltage input of 45 V.

AB - A liquid monopropellant microthruster utilizing electrolysis for ignition was designed and fabricated using low temperature co-fired ceramic tape technology. The volume of the thruster combustion chamber was 0.82 mm3. The microthruster had integrated silver electrodes to enable ignition of hydroxylammonium nitrate based liquid monopropellants by electrolytic decomposition. Energy input as small as 1.9 J produced high temperature ignition, and ignition delay times as short as 224.5 ms were achieved. A thrust output of approximately 200 mN was measured with a voltage input of 45 V.

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T3 - Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion"

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EP - 249

BT - Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion"

PB - Combustion Institute

T2 - Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007: Chemical and Physical Processes in Combustion

Y2 - 21 October 2007 through 24 October 2007

ER -

Wu MH, Yetter RA. Development and preliminary testing of an electrolytic ignition microthruster for space propulsion. 於 Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion". Combustion Institute. 2007. p. 246-249. (Fall Technical Meeting of the Eastern States Section of the Combustion Institute 2007 "Chemical and Physical Processes in Combustion").

Development and preliminary testing of an electrolytic ignition microthruster for space propulsion

摘要

出版系列

Other

All Science Journal Classification (ASJC) codes

其它文件與鏈接

指紋

引用此