• 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-1334

Lessons Learned – Cleanliness of Diaphragm Propellant Tanks (2000)

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2003

Abstract: Description of Driving Event:
The propellant tanks on the Genesis spacecraft were filled with isopropyl alcohol (IPA) prior to modal and acoustic vibration testing in order to obtain the proper spacecraft dynamic response. IPA was used as a referee fluid in place of the hydrazine propellant because of its similar mass, as well as for safety reasons. When the Genesis tanks were drained about ten days later, levels of particulate and non-volatile residue (NVR) were found that significantly exceeded the cleanliness specification. Both the particulate levels and the NVR were brought back into specification by filling the tank with IPA and draining it several times, followed by vacuum drying.
A cleanliness demonstration test was subsequently performed on an Atlas Centaur propulsion system hydrazine tank that was of a design similar to Genesis'. The Atlas tank was also found to be out-ofspecification with respect to particulate contamination. After the tank was exposed to the IPA cleaning fluid for about a day, it was also found to be out-of-specification on NVR. A total of 16 Atlas tanks were subsequently returned to the vendor.
The Genesis tank is a titanium sphere with a diaphragm fabricated from AF-E-332 rubber material. The diaphragm is incorporated to ensure gas-free propellant expulsion. When empty, the diaphragm conforms to the lower wall of the tank. As the tank is filled, the diaphragm reverses toward the upper dome of the tank. The tank is cleaned at the piece-part level and subjected to a final cleaning at the assembly level. The ability of cleaning fluids to remove particulate from the assembled tank during this final cleaning may have been limited by the fact that the vendor used only 1 liter of IPA for this procedure. Furthermore, the vendor has asserted that transportation of a "clean" tank may result in particulates being released from the faying surfaces near where the diaphragm is attached to the wall and/or in generation of particulates due to rubbing of the diaphragm on the tank wall. It is likely that the out-of-specification particulate seen in the Genesis and Atlas tanks was a result of imperfect cleaning and/or this self-generation mechanism.
Further materials testing verified that the NVR contamination was a substance leaching out of the rubber diaphragm material following prolonged exposure to IPA. This AF-E-332 diaphragm material has been used in this application since 1974, and contact with hydrazine does not produce degradation of the material or performance problems in propulsion systems. Exposure to IPA for periods of over 4 hours, however, can produce excessive NVR.
Similar tank vendor cleaning processes were used on the Deep Impact project, but it was found that conservative propulsion system filter sizing mitigated the threat of high particulate levels.
URI: http://yse.yabesh.ir/std/handle/yse/153416
Subject: alcohol flush
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (15.67Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NASA-LLIS-1334

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:30:24Z
date available2017-09-04T17:30:24Z
date copyright04/21/2003
date issued2003
identifier otherCUVEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/153416
description abstractDescription of Driving Event:
The propellant tanks on the Genesis spacecraft were filled with isopropyl alcohol (IPA) prior to modal and acoustic vibration testing in order to obtain the proper spacecraft dynamic response. IPA was used as a referee fluid in place of the hydrazine propellant because of its similar mass, as well as for safety reasons. When the Genesis tanks were drained about ten days later, levels of particulate and non-volatile residue (NVR) were found that significantly exceeded the cleanliness specification. Both the particulate levels and the NVR were brought back into specification by filling the tank with IPA and draining it several times, followed by vacuum drying.
A cleanliness demonstration test was subsequently performed on an Atlas Centaur propulsion system hydrazine tank that was of a design similar to Genesis'. The Atlas tank was also found to be out-ofspecification with respect to particulate contamination. After the tank was exposed to the IPA cleaning fluid for about a day, it was also found to be out-of-specification on NVR. A total of 16 Atlas tanks were subsequently returned to the vendor.
The Genesis tank is a titanium sphere with a diaphragm fabricated from AF-E-332 rubber material. The diaphragm is incorporated to ensure gas-free propellant expulsion. When empty, the diaphragm conforms to the lower wall of the tank. As the tank is filled, the diaphragm reverses toward the upper dome of the tank. The tank is cleaned at the piece-part level and subjected to a final cleaning at the assembly level. The ability of cleaning fluids to remove particulate from the assembled tank during this final cleaning may have been limited by the fact that the vendor used only 1 liter of IPA for this procedure. Furthermore, the vendor has asserted that transportation of a "clean" tank may result in particulates being released from the faying surfaces near where the diaphragm is attached to the wall and/or in generation of particulates due to rubbing of the diaphragm on the tank wall. It is likely that the out-of-specification particulate seen in the Genesis and Atlas tanks was a result of imperfect cleaning and/or this self-generation mechanism.
Further materials testing verified that the NVR contamination was a substance leaching out of the rubber diaphragm material following prolonged exposure to IPA. This AF-E-332 diaphragm material has been used in this application since 1974, and contact with hydrazine does not produce degradation of the material or performance problems in propulsion systems. Exposure to IPA for periods of over 4 hours, however, can produce excessive NVR.
Similar tank vendor cleaning processes were used on the Deep Impact project, but it was found that conservative propulsion system filter sizing mitigated the threat of high particulate levels.
languageEnglish
titleNASA-LLIS-1334num
titleLessons Learned – Cleanliness of Diaphragm Propellant Tanks (2000)en
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2003
contenttypefulltext
subject keywordsalcohol flush
subject keywordscleanliness verification
subject keywordsdecontamination
subject keywordsenvironmental test
subject keywordsFlight Equipment
subject keywordsHardware
subject keywordsParts Materials & Processes
subject keywordsPressure Vessels
subject keywordsSpacecraft
subject keywordsTest Article
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