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Ignition and Combustion of Metals as Fuel of Breathing Propulsion in CO_2 Planet Atmospheres

Research Project

Project/Area Number 63460072
Research Category

Grant-in-Aid for General Scientific Research (B)

Allocation TypeSingle-year Grants
Research Field Aerospace engineering
Research InstitutionTokyo Metropolitan Institute of Technology

Principal Investigator

YUASA Saburo  Tokyo Metro. Inst. Tech., Aerospace Eng., Associate Professor, 工学部, 助教授 (60123147)

Co-Investigator(Kenkyū-buntansha) NISHIYAMA Masaaki  Tokyo Metro. Inst. Tech., Aerospace Eng., Assistant, 工学部, 助手 (30099353)
GOTO Noboru  Tokyo Metro. Inst. Tech., Aerospace Eng., Assistant, 工学部, 助手 (50099363)
ISODA Hiroshi  Tokyo Metro. Inst. Tech., Aerospace Eng., Professor, 工学部, 教授 (80012186)
Project Period (FY) 1988 – 1989
Project Status Completed (Fiscal Year 1989)
Budget Amount *help
¥5,300,000 (Direct Cost: ¥5,300,000)
Fiscal Year 1989: ¥1,500,000 (Direct Cost: ¥1,500,000)
Fiscal Year 1988: ¥3,800,000 (Direct Cost: ¥3,800,000)
KeywordsPlanet Atmosphere / Jet Engine / Carbon Dioxide / Combustion / Lithium / Magnesium / Aluminum / Boron / 金属燃料 / アルミニアム / 着火 / 火炎構造 / 金属
Research Abstract

A carbon dioxide breathing turbojet engine using metals as fuel has potential for an airplane engine which can work in Mars and Venus atmospheres, consisting of CO_2. Several possible metals for this purpose are Mg, Li, Al and B, because of their high heats of reaction with CO_2. In particular, Mg and Al which have higher flame temperatures, are more attractive fuels than Li and B. The feasibility of the engine was assessed by estimating the engine performance according to thermodynamic cycle analysis. The analysis indicates that although the engine consumes a large amount of metal fuel, it gives the sufficient value of thrust.
A fundamental study was performed experimentally on the ignition and combustion of the metals in an impinging pure C0_2 gas stream. It was found that Li, Mg and Al could ignite spontaneously in t-he stream. The spontaneous ignition temperatures of Li and Mg were much lower than that of Al. The ignition process of Li had two distinct steps, first a surface reaction and then a gas phase reaction. After,ignition, Li burned in vapor-phase at first and then on the metal surface. On the other hand, at the ignition in the stream, the Mg surface was covered with a protective film against further oxidation. When initial temperatures of Mg were higher than a Critical temperature, the film formed in early reaction stages became non-protective and then gas phase reactions occurred, leading to ignition. After ignition, Mg burned in vapor-phase throughout. The ignition process of Al was found to be similar to that of Mg. However, details of the process of Al have not been made clear so far. Among these four metals, only B could not ignite in the C0_2 stream, but the reactions occurred appreciably on the surface, and the molten boron oxide appeared on its surface.

Report

(3 results)
  • 1989 Annual Research Report   Final Research Report Summary
  • 1988 Annual Research Report
  • Research Products

    (18 results)

All Other

All Publications (18 results)

  • [Publications] Yuasa,S.: "Ignition and Combustion of Small,Boron Lumps in an Oxgen Stream" Combustion and Flame(未定). (1990)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa,S.: "Ignition and Combustion of Boron Lumps in Oxygen Streams" Joint International Conference(Australia/New Zeal and Japanese Sections).The Combustion Instite. 20-22 (1989)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa,S.: "CO_2-Breathing Propulsion for a Mars Airplane" AiAA/ASME/SAE/ASEE 25th Joint Propulsion Conference. AiAA89-2863. 1-6 (1989)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] 湯浅三郎: "惑星大気中で用いるタ-ボジェットエンジンについて" タ-ボ機械. 17. 646-653 (1989)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa,S.: "Ignition and Combustion of Metals in a Carbon Dioxide Stream" The 22nd International Symposium on Combustion,The Combustion Institute. 1635-1641 (1989)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] 湯浅三郎: "火星を飛ぶジェットエンジン" 科学朝日. 3. 20-23 (1989)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa, S.: "Ignition and Combustion of Small Boron Lumps in an Oxygen Stream" Combustion and Flame, 1990.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa, S.: "Ignition and Combustion of Boron Lumps in Oxygen Streams, Joint International Conference (Australia/ New Zealand and Japanese Sections)" The Combustion Institute, 20-22, 1989.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa, S.: "CO_2-Breathing Propulsion for a Mars Airplane" AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference, AIAA 89-2863, 1989.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa, S.: "A CO_2-Breathing Turbojet Engine in Planet Atmospheres (in Japanese)" Turbomachinery, Vol.17, 646-653, 1989.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa, S.: "Ignition and Combustion of Metals in a CO_2 Stream, The 22nd International Symposium on Combustion" The Combustion Institute, 1635-1641, 1989.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa, S.: "A Jet Engine on Mars (in Japanese)" Kagaku Asahi, Vol.3, 20-23, 1989.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa, S.: "Emission Spectra of Metal-CO_2 Flames" Memoirs of Tokyo Metropolitan Institute of Technology, No.3, 25-27, 1989.

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1989 Final Research Report Summary
  • [Publications] Yuasa,S.: "Ignition and Combustion of Metals in a Carbon Dioxide Stream" The 22nd International Symposium on Combustion,The Combustion Institute. 1635-1641 (1989)

    • Related Report
      1989 Annual Research Report
  • [Publications] 湯浅三郎: "惑星大気中で用いるタ-ボジェットエンジンについて" タ-ボ機械. 17. 646-653 (1989)

    • Related Report
      1989 Annual Research Report
  • [Publications] Yuasa,S.: "CO_2ーBreathing Propulsion for a Mars Airplane" AiAA/ASME/SAE/ASEE 25th Joint Propulsion Conference. AiAA89ー2863. 1-6 (1989)

    • Related Report
      1989 Annual Research Report
  • [Publications] Yuasa,S.: "Ignition and Combustion of Boron Lumps in Oxygen Streams" Joint Internatianal Conference(Australia/New Zealand and Japanease Sections),The Combustion Institute. 20-22 (1989)

    • Related Report
      1989 Annual Research Report
  • [Publications] Yuasa,S.: "Ignition and Combustion of Small Boron Lumps in an Oxygen Stream" Combustion and Flame. (1990)

    • Related Report
      1989 Annual Research Report

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Published: 1988-04-01   Modified: 2025-11-20  

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