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/article/conceptual-design-and-preliminarily-structural-analysis-of-inflatable-basket-for-an-asteroid-capturing-satellite/>. Date accessed: 31 aug. 2024. 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/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/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. 31 Aug. 2024
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/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/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/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)
Strojniški vestnik - Journal of Mechanical Engineering 61(2015)5, 341-351
© The Authors, CC-BY 4.0 Int. Change in copyright policy from 2022, Jan 1st.
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.