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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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