Design and testing of mega-bit microthruster arrays

Koji Takahashi, Hideyo Ebisuzaki, Hayato Kajiwara, Tetsushi Achiwa, Kunihito Nagayama, Tanemasa Asano

研究成果: 著書/レポートタイプへの貢献会議での発言

10 引用 (Scopus)

抄録

Microthruster is a key for the long-term mission of nanosatellite. Micro rocket array system using solid propellant is treated theoretically and experimentally. Ignition model of energetic material is developed to understand the reaction of propellant in micro tank. It is found that there is suitable particle size of solid propellant and high heat fluence is desired. Two kinds of igniter circuits for Mega-bit microthruster are discussed and the simpler one is fabricated using MEMS technology. Successful heating of resistor in the order of 40μm is established and the reason of unstable ignition is also discussed.

元の言語英語
ホスト出版物のタイトルNanoTech 2002 - "At the Edge of Revolution"
出版物ステータス出版済み - 12 1 2002
イベントNanoTech 2002 - "At the Edge of Revolution" - Houston, TX, 米国
継続期間: 9 9 20029 12 2002

出版物シリーズ

名前NanoTech 2002 - "At the Edge of Revolution"

その他

その他NanoTech 2002 - "At the Edge of Revolution"
米国
Houston, TX
期間9/9/029/12/02

Fingerprint

Solid propellants
Ignition
Nanosatellites
Testing
Propellants
Rockets
Resistors
MEMS
Particle size
Heating
Networks (circuits)
Hot Temperature

All Science Journal Classification (ASJC) codes

  • Process Chemistry and Technology
  • Electrical and Electronic Engineering

これを引用

Takahashi, K., Ebisuzaki, H., Kajiwara, H., Achiwa, T., Nagayama, K., & Asano, T. (2002). Design and testing of mega-bit microthruster arrays. : NanoTech 2002 - "At the Edge of Revolution" (NanoTech 2002 - "At the Edge of Revolution").

Design and testing of mega-bit microthruster arrays. / Takahashi, Koji; Ebisuzaki, Hideyo; Kajiwara, Hayato; Achiwa, Tetsushi; Nagayama, Kunihito; Asano, Tanemasa.

NanoTech 2002 - "At the Edge of Revolution". 2002. (NanoTech 2002 - "At the Edge of Revolution").

研究成果: 著書/レポートタイプへの貢献会議での発言

Takahashi, K, Ebisuzaki, H, Kajiwara, H, Achiwa, T, Nagayama, K & Asano, T 2002, Design and testing of mega-bit microthruster arrays. : NanoTech 2002 - "At the Edge of Revolution". NanoTech 2002 - "At the Edge of Revolution", NanoTech 2002 - "At the Edge of Revolution", Houston, TX, 米国, 9/9/02.
Takahashi K, Ebisuzaki H, Kajiwara H, Achiwa T, Nagayama K, Asano T. Design and testing of mega-bit microthruster arrays. : NanoTech 2002 - "At the Edge of Revolution". 2002. (NanoTech 2002 - "At the Edge of Revolution").
Takahashi, Koji ; Ebisuzaki, Hideyo ; Kajiwara, Hayato ; Achiwa, Tetsushi ; Nagayama, Kunihito ; Asano, Tanemasa. / Design and testing of mega-bit microthruster arrays. NanoTech 2002 - "At the Edge of Revolution". 2002. (NanoTech 2002 - "At the Edge of Revolution").
@inproceedings{4f4a25d656b84dbc9dda3c7962b5b3fe,
title = "Design and testing of mega-bit microthruster arrays",
abstract = "Microthruster is a key for the long-term mission of nanosatellite. Micro rocket array system using solid propellant is treated theoretically and experimentally. Ignition model of energetic material is developed to understand the reaction of propellant in micro tank. It is found that there is suitable particle size of solid propellant and high heat fluence is desired. Two kinds of igniter circuits for Mega-bit microthruster are discussed and the simpler one is fabricated using MEMS technology. Successful heating of resistor in the order of 40μm is established and the reason of unstable ignition is also discussed.",
author = "Koji Takahashi and Hideyo Ebisuzaki and Hayato Kajiwara and Tetsushi Achiwa and Kunihito Nagayama and Tanemasa Asano",
year = "2002",
month = "12",
day = "1",
language = "English",
isbn = "9781624101267",
series = "NanoTech 2002 - {"}At the Edge of Revolution{"}",
booktitle = "NanoTech 2002 - {"}At the Edge of Revolution{"}",

}

TY - GEN

T1 - Design and testing of mega-bit microthruster arrays

AU - Takahashi, Koji

AU - Ebisuzaki, Hideyo

AU - Kajiwara, Hayato

AU - Achiwa, Tetsushi

AU - Nagayama, Kunihito

AU - Asano, Tanemasa

PY - 2002/12/1

Y1 - 2002/12/1

N2 - Microthruster is a key for the long-term mission of nanosatellite. Micro rocket array system using solid propellant is treated theoretically and experimentally. Ignition model of energetic material is developed to understand the reaction of propellant in micro tank. It is found that there is suitable particle size of solid propellant and high heat fluence is desired. Two kinds of igniter circuits for Mega-bit microthruster are discussed and the simpler one is fabricated using MEMS technology. Successful heating of resistor in the order of 40μm is established and the reason of unstable ignition is also discussed.

AB - Microthruster is a key for the long-term mission of nanosatellite. Micro rocket array system using solid propellant is treated theoretically and experimentally. Ignition model of energetic material is developed to understand the reaction of propellant in micro tank. It is found that there is suitable particle size of solid propellant and high heat fluence is desired. Two kinds of igniter circuits for Mega-bit microthruster are discussed and the simpler one is fabricated using MEMS technology. Successful heating of resistor in the order of 40μm is established and the reason of unstable ignition is also discussed.

UR - http://www.scopus.com/inward/record.url?scp=84862667566&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84862667566&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84862667566

SN - 9781624101267

T3 - NanoTech 2002 - "At the Edge of Revolution"

BT - NanoTech 2002 - "At the Edge of Revolution"

ER -