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Space Vehicle Mechanisms: Elements of Successful Design
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  3. Space Vehicle Mechanisms: Elements of Successful Design by Peter L. Conley - gusbestnawild.tk

The first comprehensive reference on the design, analysis, and application of space vehicle mechanisms Space Vehicle Mechanisms: Elements of Successful Design brings together accumulated industry experience in the design, analysis, and application of the mechanical systems used during space flight. It is also an excellent text for upper-level undergraduate and graduate-level courses in astronautical and mechanical engineering.

Space Vehicle Mechanisms: Elements of Successful Design brings together accumulated industry experience in the design, analysis, and application of the mechanical systems used during space flight. He has published a number of technical papers and holds several patents in areas related to space mechanisms and technology.

Space Mission Design and Operations - EPFLx on edX - Course About Video

Table of Contents Stainless Steels P. Beryllium and Its Alloys J. Structural Composites F.

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Fasterner Materials W. Ball Bearing Materials J. Spring Materials D. Solid Lubricants D.

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Other Broadly Used Materials G. Pyrotechnic Release Devices N.

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Nonexplosive Release Devices W. Ball Bearings H. Permanent Magnet Motors R. Fink, et al.

Feedback Devices T. Malcolm, et al. Rotating Signal and Power Transfer S.


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Cole, et al. Deployment Devices M. Structural Dynamics J. This paper presents a novel hinge mechanism for deployment of spacecraft subsystems such as antennas, solar arrays.

By using Axiomatic design theory, the conceptual design of the hinge mechanism is suggested, which has not only high deployed stiffness and low deployment shock but also does not require lubrication and accurate fabrication. That is, optimization of deployment torque and maximization of the deployed stiffness can be possible since this suggested hinge mechanism is decoupled design.

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Space Vehicle Mechanisms: Elements of Successful Design by Peter L. Conley - gusbestnawild.tk

And the suggested hinge mechanism is fabricated and tested to evaluate the feasibility. Quasi-static analysis is performed to optimize deployment torque for low deployment shock by using FEM. Also, the bending stiffness is measured by 4 point bending test. We use cookies to help provide and enhance our service and tailor content and ads.