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Title
  • ja オオワシ2号機推進システムに関する研究
  • en Study of Propulsion Engine for Oowashi 2
Creator
    • ja 湊, 亮二郎 ja-Kana ミナト, リョウジロウ en MINATO, Ryojiro
    • ja 東野, 和幸 ja-Kana ヒガシノ, カズユキ en HIGASHINO, Kazuyuki
    • ja 棚次, 亘弘 ja-Kana タナツグ, ノブヒロ en TANATSUGU, Nobuhiro
Accessrights open access
Rights
  • ja © 2015 室蘭工業大学
Subject
  • NDC 538
  • Other en Gas Generator Cycle Air Turboramjet Engine
  • Other en Bio Ethanol
Description
  • Other application/pdf
  • Abstract en Supersonic Unmanned Aerial Vehicle Project proceeds in Aerospace Plane Research Center at Muroran Institute Technology. The Gas Generator cycled Air Turbo Ramjet Engine is the most promising candidate for propulsion engine for this UAV. For this GG-ATR engine, its fuel and oxidizer are bio-ethanol and liquefied oxygen (LOX), respectively. The present paper describes about GG-ATR engine cycle analysis, design and manufacturing of engine components, ground test facilities. In addition, the authors describe about future study plan for ground test of GG-ATR engine.
  • Other ja 特集 : 航空宇宙機システム研究センターにおける開発研究2 : 1. オオワシII飛行にむけて並びに関連技術の研究開発(推進系)
Publisher ja 室蘭工業大学
Date
    Issued2015-03-13
Language
  • jpn
Resource Type departmental bulletin paper
Version Type VoR
Identifier HDL http://hdl.handle.net/10258/3775 , URI https://muroran-it.repo.nii.ac.jp/records/8562
Relation
  • isIdenticalTo NAID 120005594193
Journal
    • PISSN 13442708
    • NCID AA11912609
      • ja 室蘭工業大学紀要 en Memoirs of the Muroran Institute of Technology
      • Volume Number64 Page Start23 Page End28
File
    • fulltext 64_23.pdf
    • 1.2 MB (application/pdf)
      • Available2016-02-16
Oaidate 2023-10-27