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    Dynamics of Axisymmetric Rockets in Free Flight

    Source: Journal of Dynamic Systems, Measurement, and Control:;1998:;volume( 120 ):;issue: 003::page 410
    Author:
    F. O. Eke
    ,
    E. Cervantes
    DOI: 10.1115/1.2805418
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The attitude behavior of an axisymmetric, solid-propellant rocket in a torque-free environment is examined. The focus is on assessing the impact of substantial mass variation on the behavior of such systems. The main finding is that both the spin rate and the transverse angular velocity can differ substantially from those that would be observed if mass variation were neglected. The deviation is exacerbated by the presence of large amounts of propellant (variable mass) in the system. The attitude motion of such systems is also greatly influenced by the shape of the propellant grain.
    keyword(s): Dynamics (Mechanics) , Rockets , Flight , Propellants , Shapes , Torque , Motion AND Particle spin ,
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      Dynamics of Axisymmetric Rockets in Free Flight

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    http://yetl.yabesh.ir/yetl1/handle/yetl/120159
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    • Journal of Dynamic Systems, Measurement, and Control

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    contributor authorF. O. Eke
    contributor authorE. Cervantes
    date accessioned2017-05-08T23:56:06Z
    date available2017-05-08T23:56:06Z
    date copyrightSeptember, 1998
    date issued1998
    identifier issn0022-0434
    identifier otherJDSMAA-26249#410_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120159
    description abstractThe attitude behavior of an axisymmetric, solid-propellant rocket in a torque-free environment is examined. The focus is on assessing the impact of substantial mass variation on the behavior of such systems. The main finding is that both the spin rate and the transverse angular velocity can differ substantially from those that would be observed if mass variation were neglected. The deviation is exacerbated by the presence of large amounts of propellant (variable mass) in the system. The attitude motion of such systems is also greatly influenced by the shape of the propellant grain.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDynamics of Axisymmetric Rockets in Free Flight
    typeJournal Paper
    journal volume120
    journal issue3
    journal titleJournal of Dynamic Systems, Measurement, and Control
    identifier doi10.1115/1.2805418
    journal fristpage410
    journal lastpage414
    identifier eissn1528-9028
    keywordsDynamics (Mechanics)
    keywordsRockets
    keywordsFlight
    keywordsPropellants
    keywordsShapes
    keywordsTorque
    keywordsMotion AND Particle spin
    treeJournal of Dynamic Systems, Measurement, and Control:;1998:;volume( 120 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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