書誌事項
- タイトル別名
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- Ignition Characteristics of GH2/GOx Mixture Using a Laser Ablation Ignition.
- レーザーアブレーション チャッカ ホウシキ オ モチイタ スイソ サンソ コンゴウ ガス ニ オケル チャッカ トクセイ
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Irradiating a nano-second laser pulse on a solid surface, a GH2/GO2 combustion chamber was operated to measure the minimum ignition energy for three parameters: the spot diameter, the thruster pressure, and the target material. It was confirmed that this method is useful since the minimum ignition energy can be much less than that of the laser spark ignition. It turned out that the minimum ignition energy increases as the spot diameter increases, and decreases monotonously as the thruster pressure increases. In addition, it was suggested that the ignition is possible even after the irradiation of a million laser pulses by applying the metallic targets (tungsten and stainless). On the other hand, the carbon target provided poor ignition probability.
収録刊行物
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- 日本航空宇宙学会論文集
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日本航空宇宙学会論文集 50 (580), 204-209, 2002
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282679445520512
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- NII論文ID
- 10008213703
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 6170733
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
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- 使用不可