Spacecraft Structures And Mechanisms

Author: Thomas P. Sarafin
Publisher: Firefly Books
ISBN: 9780792334767
Size: 67.87 MB
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Spacecraft Structures and Mechanisms describes the integral process of developing cost-effective, reliable structures and mechanical products for space programs.

Opto Mechanical Systems Design Third Edition

Author: Paul R. Yoder, Jr.
Publisher: CRC Press
ISBN: 1420027239
Size: 79.34 MB
Format: PDF, Kindle
View: 2014
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Sarafin, T.P., Structural mechanics, in Spacecraft Structures and Mechanisms,
Sarafin, T.P. and Larson, W.J., Eds., Microcosm, Torrance and Kluwer Academic
Publishers, Boston, 1995a, chap. 4. Sarafin, T.P., Developing confidence in
mechanical designs and products, in Spacecraft Structures and Mechanisms,
Sarafin, T.P. and Larson, W.J., Eds., Microcosm, Torrance and Kluwer Academic
Publishers, Boston, 1995b, chap. 11. Sarafin, T.P., Harmel, T.A., and Webb, R.W.,
Jr., ...

Manned Spacecraft Design Principles

Author: Pasquale M Sforza
Publisher: Elsevier
ISBN: 0124199763
Size: 16.27 MB
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MSIS (1995). Man-systems integration standards. NASA STD-3000. NASA STD (
1996). Load analyses of spacecraft and payloads. NASA Technical Standard
STD-5002. Pisacane, V. L. (2005). Fundamentals of space systems (2nd ed.).
New York: Oxford. Raymer, D. P. (1989). Aircraft design—a conceptual approach.
Reston, VA: AIAA. Sarafin, T. P., & Larson, W. (1995). Spacecraft structures and
mechanisms from concept to launch, The Netherlands: Springer. Sforza, P. M. (
2012).

Advances In Reconfigurable Mechanisms And Robots I

Author: Jian S Dai
Publisher: Springer Science & Business Media
ISBN: 1447141415
Size: 50.58 MB
Format: PDF, ePub, Docs
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Deployable structure, being a kind of important structure, has become an
essential component in the spacecraft structure. Deployable mechanism can
change the main structure, secondary structure or part of the spacecraft structure
from the folded state to the unfolded state. It has been widely used for variety of
spacecraft and the planetary detector in aerospace, such as, satellite antenna,
large optical mirror, spacecraft solar array, large support structure of space
station, planetary ...

Opto Mechanical Systems Design Fourth Edition Volume 1

Author: Paul Yoder
Publisher: CRC Press
ISBN: 1482257718
Size: 58.10 MB
Format: PDF, Mobi
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Phinney, D.D. and Britton, W.P., Developing mechanisms, in Sarafin, T.P., Ed.,
Spacecraft Structures and Mechanisms, Microcosm, Inc., Torrance and Kluwer
Academic Publishers, Boston, MA, 1995, Chapter 19, p. 665. Polvani, R.S., Christ
, B.W., and Fuller, E.R. Jr., Beryllium microdeformation mechanisms, in Wilshire,
B. and Owen, D.R.J., Eds., Creep and Fracture of Engineering Materials and
Structures, Pineridge Press, Swansea, U.K., 1981. Pompea, S.M. and Breault,
R.P., Black ...

Engineering Asset Management 2016

Author: Ming J. Zuo
Publisher: Springer
ISBN: 3319622749
Size: 12.35 MB
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References. 4. 5. 6. 10. 11. Ma XR, Yu DY, Sun. 1. Chen LM (2005) Spacecraft
structures and mechanisms. China Science and Technology Press, Beijing 2. Yu
DY, Yang JZ (2011) Spacecraft mechanism technology. China Science and
Technology Press, Beijing 3. Cong Q (2012) The advance of integration
technology for space mechanisms. Spacecr Environ Eng 4:384–387 12. 13. X.
Zan (*) • S.-x.

International Aerospace Abstracts

Author:
Publisher:
ISBN:
Size: 69.12 MB
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... vehicle - Crew module study on structure, mechanisms, interfaces. T. Lorea
and L. Vanhumbeeck (Sodete Anonyme Beige de Constructions Aeronautiques,
Brussels, Belgium). In: ESA International Conference on Spacecraft Structures,
Materials and Mechanical Testing, Noordwijk, Netherlands, Mar. 27-29, 1996,
Proceedings. Vol. 3 (A97-13298 02-18). Noordwijk. Netherlands, European
Space Agency, 1996, p. 955-961. The CTV is able to transport lour persons to
and from ISSA.

Random Vibrations In Spacecraft Structures Design

Author: J. Jaap Wijker
Publisher: Springer Science & Business Media
ISBN: 9048127289
Size: 28.76 MB
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Shock loads: Deployable structures experience high shock loads; for example
during latch-up of hinges in the required final position of these mechanisms. This
is especially the case when the deployment speeds are too high. Temperatures:
Temperature variations usually cause high thermal stresses in structures. In
general, the various coefficients of expansion are accounted for in the choice of
the structural materials. Thermal deformations are taken into account when
working with ...

Spacecraft Structures

Author: J. Jaap Wijker
Publisher: Springer Science & Business Media
ISBN: 9783540755531
Size: 63.47 MB
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Acoustic loads Light structural parts with relatively large surface areas (such as
solar panels and spacecraft antennas) are more sensitive to acoustic loads than
sinusoidal and random base excitation. Shock loads Deployable structures
experience high shock loads; for example during latch-up of hinges in the
required final position of these mechanisms. This is especially the case when the
deployment velocities are too high. Temperatures Temperature variations usually
cause high ...

The Logic Of Microspace

Author: Rick Fleeter
Publisher: Springer Science & Business Media
ISBN: 9780792360285
Size: 17.16 MB
Format: PDF, ePub
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The text then goes beyond engineering technologies and management techniques to envision the tantalizing prospects microspace has in store for the industry, its present markets and those of the future.