Characteristics of Heat Transfer to Nickel Plated Chamber Walls of High Pressure Rocket Combustors

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概要

• 論文の詳細を見る
• 宇宙航空研究開発機構の論文

著者

• Kumakawa Akinaga

  National Aerospace Laboratory

• SASAKI Masaki

  National Aerospace Laboratory

• YATSUYANAGI Nobuyuki

  National Aerospace Laboratory

• Kumakawa Akinaga

  航空宇宙技術研究所

• Sakamoto Hiroshi

  National Aerospace Laboratory

関連論文

• Chemical Synthesis of Phosphorylated Peptides of The Carboxy-Terminal Domain of Human p53 by A Segment Condensation Method
• Spray and Combustion Characteristics of a Liquid-fueled Ramjet Combustor
• Spray and Combustion Characteristics of a Liquid-fueled Ramjet Combustor
• Characteristics of Heat Transfer to Nickel Plated Chamber Walls of High Pressure Rocket Combustors
• Hot Gas Side Heat Transfer Characteristics of LOX/H2 and LOX/HC Type Propellats

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