YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Applied Mechanics
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Applied Mechanics
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Minimum Transfer Time for a Power-Limited Rocket

    Source: Journal of Applied Mechanics:;1961:;volume( 028 ):;issue: 002::page 171
    Author:
    George Leitmann
    DOI: 10.1115/1.3641648
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The problem considered is that of determining the acceleration program leading to minimum transfer time for a power-limited rocket moving between prescribed positions and velocities in a constant gravitational field. It is found that flight must take place at maximum power and that the thrust-acceleration components are linear functions of time. The case of rectilinear transfer between positions of rest is treated in detail, and the results are compared with those previously obtained for a constant-acceleration transfer.
    keyword(s): Rockets , Flight , Thrust AND Functions ,
    • Download: (2.448Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Minimum Transfer Time for a Power-Limited Rocket

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/142834
    Collections
    • Journal of Applied Mechanics

    Show full item record

    contributor authorGeorge Leitmann
    date accessioned2017-05-09T00:37:02Z
    date available2017-05-09T00:37:02Z
    date copyrightJune, 1961
    date issued1961
    identifier issn0021-8936
    identifier otherJAMCAV-25616#171_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142834
    description abstractThe problem considered is that of determining the acceleration program leading to minimum transfer time for a power-limited rocket moving between prescribed positions and velocities in a constant gravitational field. It is found that flight must take place at maximum power and that the thrust-acceleration components are linear functions of time. The case of rectilinear transfer between positions of rest is treated in detail, and the results are compared with those previously obtained for a constant-acceleration transfer.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMinimum Transfer Time for a Power-Limited Rocket
    typeJournal Paper
    journal volume28
    journal issue2
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3641648
    journal fristpage171
    journal lastpage178
    identifier eissn1528-9036
    keywordsRockets
    keywordsFlight
    keywordsThrust AND Functions
    treeJournal of Applied Mechanics:;1961:;volume( 028 ):;issue: 002
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian