Generalized Vehicle Performance Closure Model for Two-Stage-to-Orbit Launch Vehicles

Generalized Vehicle Performance Closure Model for Two-Stage-to-Orbit Launch Vehicles

著者名:

Qu, M. ( Analytical Mechanics Associates, Hampton, VA )
Sohn,J.
Gage,P. ( Eloret Inc., Sunnyvale, CA )
Bradford,J. ( SpaceWorks Engineering, Atlanta, GA )
Starr,B. ( NASA Langley Research Center, Hampton, VA )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

42nd

発行年:

2004

通号:

2004-1221

ペーパー番号:

AIAA-2004-1221

出版情報:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200402 [CD-ROM 2004 Disc 2]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001598
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	42nd
会議開催地:	Reno, Nevada
会議開催年:	2004.01.05-2004.01.08

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