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A preliminary model for spacecraft propulsion performance analysis based on nuclear gain and subsystem mass-power balances

著者名:
掲載資料名:
AIAA paper
シリーズ名:
AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
シリーズ巻号:
1999
発行年:
1999
通号:
99-2838
ペーパー番号:
99-2838
開始ページ:
1
終了ページ:
11
出版情報:
American Institute of Aeronautics and Astronautics
ISSN:
01463705
言語:
英語
請求記号:
A07400
資料種別:
テクニカルペーパー

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