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NASA-STD-5012

STRENGTH AND LIFE ASSESSMENT REQUIREMENTS FOR LIQUID FUELED SPACE PROPULSION SYSTEM ENGINES

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2006

Abstract: This standard provides strength and life assessment requirements for National Aeronautics and Space Administration (NASA) liquid fueled space propulsion system engines. "Life," as used in this standard, refers to fatigue and creep. The requirements address analyses and tests to qualify an engine structurally. The total system requirements for engine hot-fire tests are not addressed in these requirements; however, a minimum number of such tests must be conducted in conjunction with structural analyses and tests to qualify the engine structurally. These requirements define the minimum structural requirements acceptable to NASA. These requirements specify analyses and test factors, margins, and other parameters where appropriate. In some cases, these requirements are expressed by reference to other standards
URI: https://yse.yabesh.ir/std/handle/yse/84096
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    NASA-STD-5012

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:20:41Z
date available2017-09-04T16:20:41Z
date copyright06/13/2006
date issued2006
identifier otherTLKSXBAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/84096
description abstractThis standard provides strength and life assessment requirements for National Aeronautics and Space Administration (NASA) liquid fueled space propulsion system engines. "Life," as used in this standard, refers to fatigue and creep. The requirements address analyses and tests to qualify an engine structurally. The total system requirements for engine hot-fire tests are not addressed in these requirements; however, a minimum number of such tests must be conducted in conjunction with structural analyses and tests to qualify the engine structurally. These requirements define the minimum structural requirements acceptable to NASA. These requirements specify analyses and test factors, margins, and other parameters where appropriate. In some cases, these requirements are expressed by reference to other standards
languageEnglish
titleNASA-STD-5012num
titleSTRENGTH AND LIFE ASSESSMENT REQUIREMENTS FOR LIQUID FUELED SPACE PROPULSION SYSTEM ENGINESen
typestandard
page25
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2006
contenttypefulltext
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DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian