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Spin rate variations of spin-stabilized apogee motors in thrust phase

Authors: V. Adimurthy; Pradeep Kumar; S. Lakshminarayanan;

Spin rate variations of spin-stabilized apogee motors in thrust phase

Abstract

Nomenclature CF = skin-friction coefficient Is = roll moment of inertia of solid Is = rate of change of 75 k = exit plane radius of gyration for roll L nozzle length m = mass flow rate r = radial distance rc = radius of forced vortex core R nozzle radius at a given section T = torque Va = axial velocity Vt = tangential velocity x = axial coordinate d>/ = initial spin rate of solid o)y = spin rate of solid, cosolid gas = effective spin rate of exhaust gases

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This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
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influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
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This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
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