Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite

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CERUTI, Alessandro ;PETTENUZZO, Siro ;TUVERI, Marco .
Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite. 
Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 61, n.5, p. 341-351, june 2018. 
ISSN 0039-2480.
Available at: <https://www.sv-jme.eu/sl/article/conceptual-design-and-preliminarily-structural-analysis-of-inflatable-basket-for-an-asteroid-capturing-satellite/>. Date accessed: 14 nov. 2019. 
doi:http://dx.doi.org/10.5545/sv-jme.2014.2063.
Ceruti, A., Pettenuzzo, S., & Tuveri, M.
(2015).
Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite.
Strojniški vestnik - Journal of Mechanical Engineering, 61(5), 341-351.
doi:http://dx.doi.org/10.5545/sv-jme.2014.2063
@article{sv-jmesv-jme.2014.2063,
	author = {Alessandro  Ceruti and Siro  Pettenuzzo and Marco  Tuveri},
	title = {Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {61},
	number = {5},
	year = {2015},
	keywords = {design; FEM analysis; inflatable structures; aerospace applications},
	abstract = {This paper presents a conceptual design of a satellite device to be used for capturing asteroids, based on inflatable structures. The mission requirements, the conceptual design, the methodology for the selection of the best solution, and simulations for the preliminarily structural analysis of the device are described within. Several finite element analyses have been carried out in order to find the best strategy to model flexible materials under internal pressure, and the device structure has been changed accordingly in order to obtain the best trade-off between weight and strength. This paper presents the sizing and the weight breakdown of the satellite inflatable components, which are quite complex to model with regards to the structural simulation. The results obtained seem to confirm the feasibility of such a structure and motivates further studies and experimental tests.},
	issn = {0039-2480},	pages = {341-351},	doi = {10.5545/sv-jme.2014.2063},
	url = {https://www.sv-jme.eu/sl/article/conceptual-design-and-preliminarily-structural-analysis-of-inflatable-basket-for-an-asteroid-capturing-satellite/}
}
Ceruti, A.,Pettenuzzo, S.,Tuveri, M.
2015 June 61. Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 61:5
%A Ceruti, Alessandro 
%A Pettenuzzo, Siro 
%A Tuveri, Marco 
%D 2015
%T Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite
%B 2015
%9 design; FEM analysis; inflatable structures; aerospace applications
%! Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite
%K design; FEM analysis; inflatable structures; aerospace applications
%X This paper presents a conceptual design of a satellite device to be used for capturing asteroids, based on inflatable structures. The mission requirements, the conceptual design, the methodology for the selection of the best solution, and simulations for the preliminarily structural analysis of the device are described within. Several finite element analyses have been carried out in order to find the best strategy to model flexible materials under internal pressure, and the device structure has been changed accordingly in order to obtain the best trade-off between weight and strength. This paper presents the sizing and the weight breakdown of the satellite inflatable components, which are quite complex to model with regards to the structural simulation. The results obtained seem to confirm the feasibility of such a structure and motivates further studies and experimental tests.
%U https://www.sv-jme.eu/sl/article/conceptual-design-and-preliminarily-structural-analysis-of-inflatable-basket-for-an-asteroid-capturing-satellite/
%0 Journal Article
%R 10.5545/sv-jme.2014.2063
%& 341
%P 11
%J Strojniški vestnik - Journal of Mechanical Engineering
%V 61
%N 5
%@ 0039-2480
%8 2018-06-27
%7 2018-06-27
Ceruti, Alessandro, Siro  Pettenuzzo, & Marco  Tuveri.
"Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite." Strojniški vestnik - Journal of Mechanical Engineering [Online], 61.5 (2015): 341-351. Web.  14 Nov. 2019
TY  - JOUR
AU  - Ceruti, Alessandro 
AU  - Pettenuzzo, Siro 
AU  - Tuveri, Marco 
PY  - 2015
TI  - Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite
JF  - Strojniški vestnik - Journal of Mechanical Engineering
DO  - 10.5545/sv-jme.2014.2063
KW  - design; FEM analysis; inflatable structures; aerospace applications
N2  - This paper presents a conceptual design of a satellite device to be used for capturing asteroids, based on inflatable structures. The mission requirements, the conceptual design, the methodology for the selection of the best solution, and simulations for the preliminarily structural analysis of the device are described within. Several finite element analyses have been carried out in order to find the best strategy to model flexible materials under internal pressure, and the device structure has been changed accordingly in order to obtain the best trade-off between weight and strength. This paper presents the sizing and the weight breakdown of the satellite inflatable components, which are quite complex to model with regards to the structural simulation. The results obtained seem to confirm the feasibility of such a structure and motivates further studies and experimental tests.
UR  - https://www.sv-jme.eu/sl/article/conceptual-design-and-preliminarily-structural-analysis-of-inflatable-basket-for-an-asteroid-capturing-satellite/
@article{{sv-jme}{sv-jme.2014.2063},
	author = {Ceruti, A., Pettenuzzo, S., Tuveri, M.},
	title = {Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {61},
	number = {5},
	year = {2015},
	doi = {10.5545/sv-jme.2014.2063},
	url = {https://www.sv-jme.eu/sl/article/conceptual-design-and-preliminarily-structural-analysis-of-inflatable-basket-for-an-asteroid-capturing-satellite/}
}
TY  - JOUR
AU  - Ceruti, Alessandro 
AU  - Pettenuzzo, Siro 
AU  - Tuveri, Marco 
PY  - 2018/06/27
TI  - Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite
JF  - Strojniški vestnik - Journal of Mechanical Engineering; Vol 61, No 5 (2015): Strojniški vestnik - Journal of Mechanical Engineering
DO  - 10.5545/sv-jme.2014.2063
KW  - design, FEM analysis, inflatable structures, aerospace applications
N2  - This paper presents a conceptual design of a satellite device to be used for capturing asteroids, based on inflatable structures. The mission requirements, the conceptual design, the methodology for the selection of the best solution, and simulations for the preliminarily structural analysis of the device are described within. Several finite element analyses have been carried out in order to find the best strategy to model flexible materials under internal pressure, and the device structure has been changed accordingly in order to obtain the best trade-off between weight and strength. This paper presents the sizing and the weight breakdown of the satellite inflatable components, which are quite complex to model with regards to the structural simulation. The results obtained seem to confirm the feasibility of such a structure and motivates further studies and experimental tests.
UR  - https://www.sv-jme.eu/sl/article/conceptual-design-and-preliminarily-structural-analysis-of-inflatable-basket-for-an-asteroid-capturing-satellite/
Ceruti, Alessandro, Pettenuzzo, Siro, AND Tuveri, Marco.
"Conceptual Design and Preliminarily Structural Analysis of Inflatable Basket for an Asteroid Capturing Satellite" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 61 Number 5 (27 June 2018)

Avtorji

Inštitucije

  • University of Bologna, Industrial Engineering Department - DIN, Italy 1
  • University of Bologna, School of Engineering and Architecture, Italy 2
  • University of Bologna, Interdepartmental Centre for Industrial Research in Aeronautics, Italy 3

Informacije o papirju

Strojniški vestnik - Journal of Mechanical Engineering 61(2015)5, 341-351

https://doi.org/10.5545/sv-jme.2014.2063

This paper presents a conceptual design of a satellite device to be used for capturing asteroids, based on inflatable structures. The mission requirements, the conceptual design, the methodology for the selection of the best solution, and simulations for the preliminarily structural analysis of the device are described within. Several finite element analyses have been carried out in order to find the best strategy to model flexible materials under internal pressure, and the device structure has been changed accordingly in order to obtain the best trade-off between weight and strength. This paper presents the sizing and the weight breakdown of the satellite inflatable components, which are quite complex to model with regards to the structural simulation. The results obtained seem to confirm the feasibility of such a structure and motivates further studies and experimental tests.

design; FEM analysis; inflatable structures; aerospace applications