書誌事項
- タイトル別名
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- F217 Study for the Space Craft for Interplanetary Cruise
説明
We considered that the nuclear power is proper for the energy source of the manned spacecraft for interplanetary cruise. In this study, we considered the navigational plan to reach Mars, the size of power generating system and if that was reasonable. The spacecraft studied in our laboratory has a Fast Breeder Reactor with liquid sodium as main heat source, Stirling Engines as power generators and some Variable Specific Impulse Magnetroprasma Rockets (VASIMR) as propulsion system. To obtain the optimal trajectory of rapid Mars transit, we made an analysis program that analyzes the optimal time-history of acceleration which realizes smaller duration and greater payload mass. If payload mass is low (100[ton]), the spacecraft can reach Mars in 4 or 5 months with comparatively-less power. In these cases, whose sizes of reactor are reasonable to load on the spacecraft.
収録刊行物
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- 動力・エネルギー技術の最前線講演論文集 : シンポジウム
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動力・エネルギー技術の最前線講演論文集 : シンポジウム 2008.13 (0), 517-518, 2008
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390282680863810944
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- NII論文ID
- 110007704045
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- ISSN
- 24242950
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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
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可