Free Attitude Motions of a Spinning Body With Substantial Mass Loss-Reference-Cited by-同舟云学术

Free Attitude Motions of a Spinning Body With Substantial Mass Loss

Published:2004-03-01 Issue:2 Volume:71 Page:190-194
ISSN:0021-8936
Container-title:Journal of Applied Mechanics
language:en
Short-container-title:

Author:

Eke Fidelis O.¹,Mao Tai-Chien²,Morris Michael J.³

Affiliation:

1. Department of Mechanical and Aeronautical Engineering, University of California, Davis, Davis, CA 95616

2. Northrup Grumman Electronics Systems, 1100 West Hollyvale Street, Azusa, CA 91702

3. Lockheed-Martin Space Systems Company, 1111 Lockheed Martin Way, Sunnyvale, CA 94089

Abstract

This paper explores the various analytical links between the free attitude motions of spinning bodies of the rocket type, and the system’s parameters. The system is modeled as an axisymmetric body with substantial mass loss, and special attention is paid to the presence of a nozzle on the system. It is found that the nozzle expansion ratio can have an important influence on attitude motion, the higher this ratio the better behaved the system.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Link

http://asmedigitalcollection.asme.org/appliedmechanics/article-pdf/71/2/190/5470631/190_1.pdf

Reference13 articles.

1. Gilmore, A. W., and Keller, T. L., 1957, “Damping due to Internal Flow,” J. Aeronaut. Sci., 24(4) pp. 317–318.

2. Rott, N., and Pottsepp, L., “Simplified Calculation of the Jet Damping Effects,” AIAA J., 2(4), pp. 764–766.

3. Breuer, D. W., and Southerland, W. E., 1965, “Jet Damping Effects: Theory and Experiment,” J. Spacecr. Rockets, 2(4), pp. 638–639.

4. Thomson, W. T., and Reiter, G. S., 1965, “Jet Damping of a Solid Rocket: Theory and Flight Results,” AIAA J., 3(3), pp. 413–417.

5. Warner, G. G., and Snyder, V. M., 1968, “A Re-evaluation of Jet Damping,” J. Spacecr. Rockets, 5(3), pp. 364–366.

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Geometry of motion and nutation stability of free axisymmetric variable mass systems;Nonlinear Dynamics;2018-07-26

2. Approximate Solution to the Angular Speeds of a Nearly-Symmetric Mass-Varying Cylindrical Body;The Journal of the Astronautical Sciences;2016-11-28

3. Modeling of aircraft with time-varying inertia properties;AIAA Modeling and Simulation Technologies Conference;2015-01-02

4. Modeling and Simulation of Flight Dynamics of Supersonic Inflatable Advanced Decelerator;AIAA/AAS Astrodynamics Specialist Conference;2014-08-01

5. A Modified Analysis of Alternate Lateral Trimming Methods for Flying Wing Aircraft at Sweet Spot in Formation Flight;AIAA Atmospheric Flight Mechanics Conference;2014-01-10