A preliminary model for spacecraft propulsion performance analysis based on nuclear gain and subsystem mass-power balances AIAA-99-2838

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

AIAA-99-2838

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Material Type: 規格・テクニカルリポート類
Title: A preliminary model for spacecraft propulsion performance analysis based on nuclear gain and subsystem mass-power balances
Author/Editor: Chakrabarti, S
Schmidt, G. R
Thio, Y. C
Hurst, C. M
Publication Date: 1999
Publication Date (W3CDTF): 1999
Extent: 11 p
Alternative Title: AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit. 35th. Los Angeles, Calif. Jun. 1999
Report No.: テクニカルリポート番号 : AIAA-99-2838
Holding library: 国立国会図書館
Call No.: M-AIAA-99-2838
Data Provider (Database): 国立国会図書館 : 国立国会図書館蔵書
https://ndlsearch.ndl.go.jp
Bibliographic ID (NDL): 000005897006
http://id.ndl.go.jp/bib/000005897006
Bibliographic Record Category (NDL): 291