Failure Analyses of Idle Spin Phenomena in Liquid Hydrogen Pumps for Rocket Engines
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- Hirata Kunio
- 宇宙航空研究開発機構角田エンジン開発室
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- Kamijo Kenjiro
- 元 東北大学流体科学研究所
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- Masuya Goro
- 東北大学大学院工学研究科
Bibliographic Information
- Other Title
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- ロケット用液化水素ポンプの過渡時に発生する空転現象の解明
- ロケットヨウ エキカ スイソ ポンプ ノ カトジ ニ ハッセイ スル クウテン ゲンショウ ノ カイメイ
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Abstract
Idle spin phenomena were observed at rapid transient phase in liquid hydrogen pumps for rocket engines. Failure analyses were conducted and evaluation equations to estimate the shift of the operation point of the pump were derived in this paper. It was revealed that rapid fall of hydrogen flow rate resulted in decrease of pump efficiency which caused excessive temperature rise up to the saturation of the pump fluid.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 53 (614), 123-129, 2005
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390001204470328960
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- NII Article ID
- 10015421567
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 7286468
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed