Development and investigation of transformable-volume structures for space applications

1Lobanov, LM, 2Volkov, VS
1E.O. Paton Electric Welding Institute of the National Academy of Sciences of Ukraine, Kyiv, Ukraine
2E. O. Paton Electric Welding Institute, Kyiv, Ukraine
Kosm. nauka tehnol. 2015, 21 ;(4):32–38
https://doi.org/10.15407/knit2015.04.032
Section: Space Instruments
Publication Language: Ukrainian
Abstract: 

We present a grounded optimal type of transformable-volume structures’ (TVS) basic surface and the developed mathematical model of its transformation into a compact form. Optimal geometric parameters of a conical type TVS were determined. The parameters of stresses distribution in a structure’s shell at successive stages of transformation was modeled and kinetics of a thinwalled conical TSV unfolding process was studied. Quality criteria of permanent joints of the transformable thin-walled metal shells were determined and the technological equipment for their manufacture and laboratory tests samples was designed.

Keywords: deployable space structures, load-carrying shells, transformable-volume structures
References: 

1. Volkov V. On isometries of surfaces of revolution.  Visnyk KNU. Ser. Matematyka. Mehanika. No. 29, 36—39 (2013) [in Ukrainian].

2.  Paton B. E., Gvozdeckij V. S., Dudko D. A. et al. Microplasma welding [Mikroplazmennaja svarka].  248 p. (Nauk. dumka, Kiev, 1979) [in Russian].

3.  Paton B. E., Lobanov L. M., Volkov V. S. Transformable structures (Review).  The Paton Welding J.  12, 25—33 (2011).

4.  Schenk M., Viquerat A. D., et. al. Review of Inflatable Booms for Deployable Space Structures: Packing and Rigidization.  J. Spacecraft and Rockets. 51 (3),  (2014) Retrieved from http://wwwg.eng.cam.ac.uk/advancedstructuresfiles/pdf/2014JSR.pdf

DOI: 10.2514 /1.A32598,