SPACE SHUTTLE MAIN ENGINE POWERHEAD STRUCTURAL MODELING, STRESS AND FATIGUE LIFE ANALYSIS VOLUME 2 - STRESS SUMMARY OF BLADES AND NOZZLES AT FPL AND 115 PERCENT RPL LOADS - SSME HPFTP AND HPOTP BLADES AND NOZZLES

SPACE SHUTTLE MAIN ENGINE POWERHEAD STRUCTURAL MODELING, STRESS AND FATIGUE LIFE ANALYSIS VOLUME 2 - STRESS SUMMARY OF BLADES AND NOZZLES AT FPL AND 115 PERCENT RPL LOADS - SSME HPFTP AND HPOTP BLADES AND NOZZLES

著者名:

Hammett, J. C. ( Lockheed Missiles & Space Company, Inc. )

Price, J. M. ( Lockheed Missiles & Space Company, Inc. )

Robinson, J. K. ( Lockheed Missiles & Space Company, Inc. )

Teal, G. A. ( Lockheed Missiles & Space Company, Inc. )

Thomson, J. M. ( Lockheed Missiles & Space Company, Inc. )

Tilley, D. M. ( Lockheed Missiles & Space Company, Inc. )

Welch, C. T. ( Lockheed Missiles & Space Company, Inc. )

さらに 2 件

掲載資料名:

NASA Technical Reports

発行年:

1983

号:

NASA-CR-171001

通号:

G3/20 18782

パート:

NAS 1.26:171001

ペーパー番号:

N84-20637

開始ページ:

1

終了ページ:

443

総ページ数:

443

出版情報:

National Aeronautics and Space Administration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:

ZA00002949

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