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  1. 掲載誌一覧
  2. 鹿児島大学工学部研究報告
  3. vol.59
  1. 工学部
  2. 工学部・紀要論文

ハイブリッドロケットエンジンの気体噴射用インジェクターの流路断面積について

http://hdl.handle.net/10232/00029946
http://hdl.handle.net/10232/00029946
b246d2a0-a009-46ec-88ac-a6fab53b8fef
名前 / ファイル ライセンス アクション
No59-01.pdf No59-01 (2.3 MB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2018-01-05
タイトル
タイトル ハイブリッドロケットエンジンの気体噴射用インジェクターの流路断面積について
タイトル
タイトル言語 en
タイトル Cross-sectional Area of Oxidizer-gas Injector of Hybrid Rocket Engines
タイトルよみ
タイトルよみ ハイブリッド ロケット エンジン ノ キタイ フンシャヨウ インジェクター ノ リュウロ ダンメンセキ ニツイテ
著者 片野田, 洋

× 片野田, 洋

WEKO 128720

片野田, 洋

Search repository
著者よみ
姓名 カタノダ, ヒロシ
別言語の著者
姓名 KATANODA, Hiroshi
言語
言語 jpn
キーワード
主題言語 en
主題Scheme Other
主題 Hybrid Rocket
キーワード
主題言語 en
主題Scheme Other
主題 Gaseous Oxidizer
キーワード
主題言語 en
主題Scheme Other
主題 Cross-sectional Area
キーワード
主題言語 en
主題Scheme Other
主題 Injector
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_6501
資源タイプ departmental bulletin paper
要約(Abstract)
内容記述タイプ Other
内容記述 A cross-sectional area of oxidizer-gas injector of a hybrid rocked engines, required no to be choked at the injector, is theoretically calculated. The calculation is based on steady quasi-one-dimensional isentropic flow upstream of the injector exit and chemical equilibrium analysis in a combustion chamber of the hybrid rocked engine. The calculation is conducted for PMMA as fuel and gaseous oxygen as oxidizer. Under the specific conditions of the injector pressure is 0.8MPa, combustion gas pressure is 0.75MPa, design Mach number of the nozzle is 2.0, and the nozzle throat diameter is 11.8mm, each of four injectors must be 4.6mm or more in diameter, in order to avoid choking.
収録雑誌名 鹿児島大学工学部研究報告

巻 59, p. 1-4, 発行日 2017-12
ISSN
収録物識別子タイプ ISSN
ISSN 0451212X
NII書誌ID(雑誌)
収録物識別子タイプ NCID
NC ID AN00040363
出版タイプ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
NDC
主題Scheme NDC
主題 538
公開者・出版者
出版者 鹿児島大学
公開者よみ
公開者よみ カゴシマ ダイガク
公開者別名
公開者別名 Kagoshima University
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