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Featured researches published by Nobuyuki Yatsuyanagi.


Advanced Materials '93#R##N#Ceramics, Powders, Corrosion and Advanced Processing | 1994

ZrO2/Ni composite plating for high pressure thrust chambers

Akinaga Kumakawa; Nobuyuki Yatsuyanagi; Hiroshi Sakamoto

The chamber wall of a water-cooled calorimetric rocket combustor was electroplated with ZrO2 dispersed nickel. Combustion tests were conducted using liquid oxygen/gaseous hydrogen at a chamber pressure of 7 MPa. The structural integrity and performance of the composite plating as a thermal barrier were examined.


Archive | 1987

Rocket combustion chamber cooling wall of composite cooling type and method of manufacturing the same

Masayuki Niino; Nobuyuki Yatsuyanagi; Akiraga Kumakawa; Akio Suzuki; Hiromi Gomi; Hiroshi Sakamoto; Masaki Sasaki; Yoshimichi Masuda; Ryuzo Watanabe; Junjiro Takekawa; Etsuo Ohtsuki; Terashi Isago


23rd Joint Propulsion Conference | 1987

LOX/methane staged combustion rocket combustor investigation

Hiroshi Tamura; Fumiei Ono; Akinaga Kumakawa; Nobuyuki Yatsuyanagi


Archive | 1992

Experimental study on liquid methane cooled thrust chambers

Akinaga Kumakawa; Masaki Sasaki; Mamoru Takahashi; Kazuo Sato; Hiroshi Sakamoto; Fumiei Ono; Nobuyuki Yatsuyanagi; Kazuo Sano; Kazuyuki Higashino


Archive | 1983

Method of manufacturing a rocket combustion chamber

Masayuki Niino; Nobuyuki Yatsuyanagi; Akinaga Kumakawa; Akio Suzuki; Hiromi Gomi; Hiroshi Sakamoto; Masaki Sasaki; Yoshimichi Masuda; Ryuzo Watanabe; Junjiro Takekawa; Etsuo Ohtsuki; Terashi Isago


航空宇宙技術研究所報告 | 1990

Hot Gas Side Heat Transfer Characteristics of LOX/H2 and LOX/HC Type Propellats

Akinaga Kumakawa; Masaki Sasaki; Kazuo Sato; Hiroshi Tamura; Fumiei Ono; Hiroshi Sakamoto; Nobuyuki Yatsuyanagi; 彰長 熊川; 正樹 佐々木; 和雄 佐藤; 洋 田村; 文衛 小野; 博 坂本; 信之 八柳


Transactions of The Japan Society for Aeronautical and Space Sciences | 2009

Establishment of Design Method for Liquid Hydrogen Regenerative Cooling Combustor of LOX/Hydrogen Rocket Engine

Nobuyuki Yatsuyanagi


Atomization and Sprays | 1994

ATOMIZATION CHARACTERISTICS OF LIQUID JETS INJECTED INTO A HIGH-VELOCITY FLOW FIELD

Nobuyuki Yatsuyanagi; Hiroshi Sakamoto; Kazuo Sato


Archive | 1982

An Experimental and Analytical Study on Spray Flow Field by Liquid/Gas Coaxial Injector Elements(1)

Nobuyuki Yatsuyanagi; 信之 八柳


Transactions of The Japan Society for Aeronautical and Space Sciences | 2009

Comprehensive Design Method for LOX/Liquid-Methane Regenerative Cooling Combustor with Coaxial Injector

Nobuyuki Yatsuyanagi

Collaboration


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Hiroshi Sakamoto

National Aerospace Laboratory

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Akinaga Kumakawa

National Aerospace Laboratory

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Masaki Sasaki

Japan Aerospace Exploration Agency

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Masayuki Niino

National Aerospace Laboratory

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Akio Suzuki

National Aerospace Laboratory

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Hiromi Gomi

National Aerospace Laboratory

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Fumiei Ono

Japan Aerospace Exploration Agency

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Kazuo Sato

National Aerospace Laboratory

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Ryuzo Watanabe

National Aerospace Laboratory

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Etsuo Ohtsuki

National Aerospace Laboratory

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