• 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-1861

Lessons Learned – TWT using WR-34 waveguide for K-band operation

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2010

Abstract: Abstract:
It was necessary to use a WR34 waveguide for the Lunar Reconnaissance Orbiter (LRO) traveling wave tube amplifier (TWTA) because the operating frequency would be 25.65 GHz, and the existing WR28 waveguide could not be used at this frequency. Because the WR34 is a bigger waveguide, it could potentially be flown on future missions such as a Tracking and Data Relay Satellite (TDRS) or other near-Earth mission.
URI: https://yse.yabesh.ir/std/handle/yse/52501
Subject: Engineering Design (Phase C/D).Spacecraft and Spacecraft Instruments
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (13.43Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NASA-LLIS-1861

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:49:31Z
date available2017-09-04T15:49:31Z
date copyright01/29/2010
date issued2010
identifier otherBDGIQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/52501
description abstractAbstract:
It was necessary to use a WR34 waveguide for the Lunar Reconnaissance Orbiter (LRO) traveling wave tube amplifier (TWTA) because the operating frequency would be 25.65 GHz, and the existing WR28 waveguide could not be used at this frequency. Because the WR34 is a bigger waveguide, it could potentially be flown on future missions such as a Tracking and Data Relay Satellite (TDRS) or other near-Earth mission.
languageEnglish
titleNASA-LLIS-1861num
titleLessons Learned – TWT using WR-34 waveguide for K-band operationen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2010
contenttypefulltext
subject keywordsEngineering Design (Phase C/D).Spacecraft and Spacecraft Instruments
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