Axial Thrust Balancing of the LE-7 LOX Turbopump
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概要
- 論文の詳細を見る
- 1995-05-04
著者
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YOSHIDA Makoto
National Food Research Institute
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Hasegawa Satoshi
National Aerospace Laboratory
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SHIMURA Takashi
Turbopump Section, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
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Shimura Takashi
Turbopump Section Institute Of Aerospace Technology Japan Aerospace Exploration Agency
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Shimura Takashi
National Aerospace Laboratory Kspl
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Watanabe Mitsuo
Turbopump Section Institute Of Aerospace Technology Japan Aerospace Exploration Agency
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WATANABE Mitsuo
National Aerospace Laboratory, Kakuda Research Center
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Yoshida Makoto
National Aerospace Laboratory Kspl
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Hasegawa Satoshi
Turbopump Section Institute Of Aerospace Technology Japan Aerospace Exploration Agency
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Yoshida Makoto
National Aerospace Laboratory Kakuda Research Center
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- Ripple Shielding for Accurate Resistivity Measurements in Hybrid Magnets(Part II. Several Instruments and Techniques Developed in HFLSM)
- Unsteady Pressure Fluctuations in an Inducer
- A Rotating Stall Type Phenomenon Caused by Cavitation in LE-7A LH2 Turbopump
- Axial Thrust Balancing of the LE-7 LOX Turbopump