• 0
    • ارسال درخواست
    • حذف همه
    • Industrial Standards
    • Defence Standards
  • درباره ما
  • درخواست موردی
  • فهرست استانداردها
    • Industrial Standards
    • Defence Standards
  • راهنما
  • Login
  • لیست خرید شما 0
    • ارسال درخواست
    • حذف همه
View Item 
  •   YSE
  • Defence Standards
  • NASA - National Aeronautics and Space Administration (NASA)
  • View Item
  •   YSE
  • Defence Standards
  • NASA - National Aeronautics and Space Administration (NASA)
  • View Item
  • All Fields
  • Title(or Doc Num)
  • Organization
  • Year
  • Subject
Advanced Search
JavaScript is disabled for your browser. Some features of this site may not work without it.

Archive

NASA-LLIS-0033

Lessons Learned - External Tank (ET) Vent System Withdrawal Weight Securing Device

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1992

Abstract: Description of Driving Event:
The 1500-pound withdrawal weight for the ET LH2 vent line must be raised to access the withdrawal weight shock absorbers to perform maintenance. Personnel work directly beneath the withdrawal weight, held in place with a 125 psi air-operated winch and 5/8" diameter wire rope. The system design does not include a secondary means to secure the weight if the winch or wire rope fails, so workers shore the weights with pieces of wood or other available material that will brace the weights. The improperly used shoring devices could break under the load of the weights, causing injury to personnel.
URI: https://yse.yabesh.ir/std/handle/yse/52398
Subject: Facilities
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (13.07Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NASA-LLIS-0033

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:49:26Z
date available2017-09-04T15:49:26Z
date copyright09/17/1992
date issued1992
identifier otherQDYCQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/52398
description abstractDescription of Driving Event:
The 1500-pound withdrawal weight for the ET LH2 vent line must be raised to access the withdrawal weight shock absorbers to perform maintenance. Personnel work directly beneath the withdrawal weight, held in place with a 125 psi air-operated winch and 5/8" diameter wire rope. The system design does not include a secondary means to secure the weight if the winch or wire rope fails, so workers shore the weights with pieces of wood or other available material that will brace the weights. The improperly used shoring devices could break under the load of the weights, causing injury to personnel.
languageEnglish
titleNASA-LLIS-0033num
titleLessons Learned - External Tank (ET) Vent System Withdrawal Weight Securing Deviceen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1992
contenttypefulltext
subject keywordsFacilities
subject keywordsGround Equipment
subject keywordsGround Operations
subject keywordsHardware
subject keywordsIndustrial Operations
subject keywordsLaunch Process
subject keywordsLaunch Vehicle
subject keywordsLifting Devices
subject keywordsSafety & Mission Assurance
DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian
 
DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian