GOVERNING EQUATIONS IN MECHANICAL ANALYSIS OF SATELLITE CARRIER ADAPTER

Q: How can I download an article?

To download an article from SID, first log in to the site, search for the article title, and click on the 'Download Article' option.

Q: How can I download an ISI article?

To download an ISI article on SID, enter the keyword or article title in the search bar, view the relevant results, click on the desired article, and select the 'Download Article' option.

Q: How can I access the SID database?

To access the SID database, visit SID.ir, create an account, and log in to access scientific resources.

Q: Is downloading articles from SID free?

Some articles on SID are available for free, while others require payment. Details are specified on the article's page.

ESKANDARI JAM J.; NOORABADI M.; TAGHAVIAN S.H.; GARSHASBI NIA N.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: Journal of Space Science and Technology Year:2012 | Volume:5 | Issue:1 Page(s): 41-50

Download Full-Text

Persian Verion

View:

704

Download:

Cites:

Information Journal Paper

Title

GOVERNING EQUATIONS IN MECHANICAL ANALYSIS OF SATELLITE CARRIER ADAPTER

Author(s)

ESKANDARI JAM J. | NOORABADI M. | TAGHAVIAN S.H. | GARSHASBI NIA N. | Issue Writer Certificate

Keywords

CARRIER ADAPTERQ2

COMPOSITE LATTICE SHELLQ2

RIBQ2

FEMQ2

Abstract

In this paper the mechanical behavior of satellite CARRIER ADAPTER made of COMPOSITE LATTICE SHELL is examined. First, the geometrical parameters of the COMPOSITE LATTICE SHELL are analyzed. Choosing the direction for winding the fibers (geodesic route), geometric equations of the structure is elicited. Then, stiffness matrix of the structure is obtained according to these equations. Finally using finite element modeling of a conical lattice shell sample, the comparison between finite element and analytical results are presented. The analytical and numerical results show that with increasing RIB's thickness and Width, axial strain of the structure decreases nonlinearly.

Cites

No record.

References

No record.

Cite

APA: Copy

ESKANDARI JAM, J., NOORABADI, M., TAGHAVIAN, S.H., & GARSHASBI NIA, N.. (2012). GOVERNING EQUATIONS IN MECHANICAL ANALYSIS OF SATELLITE CARRIER ADAPTER. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 5(1), 41-50. SID. https://sid.ir/paper/149905/en

Vancouver: Copy

ESKANDARI JAM J., NOORABADI M., TAGHAVIAN S.H., GARSHASBI NIA N.. GOVERNING EQUATIONS IN MECHANICAL ANALYSIS OF SATELLITE CARRIER ADAPTER. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2012;5(1):41-50. Available from: https://sid.ir/paper/149905/en

IEEE: Copy

J. ESKANDARI JAM, M. NOORABADI, S.H. TAGHAVIAN, and N. GARSHASBI NIA, “GOVERNING EQUATIONS IN MECHANICAL ANALYSIS OF SATELLITE CARRIER ADAPTER,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 5, no. 1, pp. 41–50, 2012, [Online]. Available: https://sid.ir/paper/149905/en

Related Journal Papers