TECHNICAL PAPERS
Jun 15, 2004

Investigation of Geometric Imperfection in Inflatable Aerospace Structures

Publication: Journal of Aerospace Engineering
Volume 17, Issue 3

Abstract

Communication and solar array inflated structures must be deployed to a very precise geometric configuration in order to meet quality requirements of their application. The focus of this paper is on geometric imperfections associated with inflated structures. To further understand some of the elements, that derive imperfection in a parabolic inflated communication and solar array structures, a computational model is proposed. This computational approach is dictated by the geometric complexity, deformation sensitivity as function of load and boundary conditions, and nonlinear characteristics of inflated structure assemblies. The deformation of a single component depends on the flexibility/stiffness of other components due to their interaction. In order to simulate such deformations of the multicomponent inflated structure, in the present study, the computational model consists of main parabolic shape envelope (reflector and canopy), torus, and catenary’s support and uses geometric nonlinear finite element. Further, tuning of communications and solar arrays is a primary concern in the operation of these systems. To investigate the effects of pressure tuning on geometric imperfection of a parabolic inflated antenna, in this investigation, analyses using uniformly axisymmetric and asymmetric applied load are performed. The analyses assume an initial parabolic shape envelope with a perfect circular edge for the reflector and canopy. Error estimates, which quantify geometric imperfections, are computed. The results show that as the axisymmetric load increases, the surface deviation from the parabolic shape of the envelope also increases. An asymmetric load on the surface of the torus leads to variable tensile forces in the catenary along the circular edge of the envelope, which in turn cause a visible local asymmetrical deformation in the vicinity of the circular edge of the envelope. In general, an asymmetric load causes greater geometric imperfections and should be avoided

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References

ABAQUS. (1995). ABAQUS/Standard Version 4.5, Hibbitt, Karlsson, and Sorensen, Providence, R.I.
Bishop, J. A. (1998). “Shape correction of initially flat membranes by a genetic algorithm.” The 39th AIAA/ASME/ASCE/AHS/ASC, Structure, Structure Dynamics, and Materials Conf., AIAA, 98-1984.
Fichter, W. B.(1984). “Reduction of root-mean-square error in faceted antennas.” AIAA J., Spacecraft, 22, 1679–1684.
Foppl, A. (1970). Vorlesungen uber technische mechanik, B. G. Teubner, Bd. 5, Leipzig, Germany, 132–136.
Freeland, R. E., and Bilyeu, G. (1992). “In-step inflatable antenna experiment, The World Space Congress 1992.” 43rd Congress of the Int. Astronautical Federation, International Astronautical Federation, 3–5, Rue Mario-Nikis, 75015 Paris, LAF-92-0301.
Greschik, G., and Mikulas, M. M. (1996). “On imperfections and stowage creases in aluminum-rigidized inflated cylinders.” The 37th AIAA/ASME/ASCE/AHS/ASC, Structure, Structure Dynamics, and Materials Conf., AIAA, 96-1332.
Greschik, G., Mikulas, M. M., and Palisoc, A. (1998a). “Approximations and errors in pressurized axisymmetric membrane shape predictions.” The 39th AIAA/ASME/ASCE/AHS/ASC, Structure, Structure Dynamics, and Materials Conf., AIAA, 98-2101-CP.
Greschik, G., Palisoc, A., Veal, G., Cassapakis, C., and Mikulas, M. M. (1998b). “Approximating paraboloids with axisymmetric pressurized membranes.” The 39th AIAA/ASME/ASCE/AHS/ASC, Structure, Structure Dynamics, and Materials Conf., AIAA, 98-2102-CP.
Hencky, H.(1915). “Uber den spannungszustand in kreisrunden platten.” Z. Math Phys., 63, 311–317.
Jenkins, C. H., and Marker, D. K. (1998). “Improved surface accuracy of precision membrane reflectors through adaptive rim control.” The 39th AIAA/ASME/ASCE/AHS/ASC, Structure, Structure Dynamics, and Materials Conf., AIAA, 98-1983-CP.
Jenkins, C. H., Kalanovic, V. D., Padmanabhan, K., and Faisal, S. M.(1998). “Intelligent shape control for precision membrane antenna and reflectors in space.” Smart Mater. Struct., 8, 857–867.
Malone, P. K., Crawford, L., and Williams, G. T. (1993). “Developing an inflatable solar array.” 7th AIAA/USU Conf. on Small Satellites, LPA-93-GW-008, P1J93, UT.
Meyer, R. X.(1985). “Precision of mesh-type reflectors for large space-borne antennas.” J. Spacecraft, 22, 80–84.
Mikulas, M. M., and Cassapakis, C. (1995). “Rigidizable structural concepts for the new generation of small spacecraft.” The 36th AIAA/ASME/ASCE/AHS/ASC Structure, Structure Dynamics, and Materials Conf., AIAA 95-1277-CP.
Moore, J. D., and Bishop, J. A. (1998). “Evaluation of catenary suspension for reducing shape errors in inflated solar concentrators.” The 39th AIAA/ASME/ASCE/AHS/ASC, Structure, Structure Dynamics, and Materials Conf., AIAA, 98-1985-CP.
Natori, M. C., Higuchi, K., Sekine, K., and Okazaki, K., (1994). “Advanced concepts of inflatable rigidized structures for space applications.” The 35th AIAA/ASME/ASCE/AHS/ASC Structure, Structure Dynamics, and Materials Conf., AIAA, 94–1473.
Reibaldi G., Hammer, J., Bernasconi, M. C., and Pagana, E. (1986). “Inflatable space rigidized reflector development for land mobile missions.” Proc., Communications Satellite Systems Conf., AIAA, 533–538.
Ruze, J.(1967). “Antenna tolerance theory—A review.” Proc. IEEE, 54, 633–640.
Salama, M., Kuo, C. P., Garba, J., Wada, B., and Thomas, M. (1994). “On-orbit shape correction of inflatable structures.” AIAA Conf. Adaptive Structures, AIAA, 94–1771.
Utku, S., Kuo, C. P., Garba, J. A., and Wada, B. K.(1995). “Shape control of inflatable reflectors.” J. Intell. Mater. Syst. Struct., 6, 550–556.
von Karman, T. (1910). “Festigkeitsproblem in naschinenbau.” Encyk D Math Wiss IV, 311–385.
Zarghamee, M. S.(1967). “On antenna tolerance theory.” IEEE Trans. Antennas Propag., 15, 777–781.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 17Issue 3July 2004
Pages: 98 - 105

History

Received: Jan 30, 2003
Accepted: Oct 30, 2003
Published online: Jun 15, 2004
Published in print: Jul 2004

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Authors

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S. Naboulsi
Professor, Dept. of Aeronautics and Astronautics, Air Force Institute of Technology (AFIT/ENY) Wright–Patterson Air Force Base, OH 45433-7765.

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