Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Luisa Boni"'
Publikováno v:
Aerospace, Vol 11, Iss 2, p 151 (2024)
Photonic solar sails are a class of advanced propellantless propulsion systems that use thin, large, lightweight membranes to convert the momentum of light from the Sun into thrust for space navigation. The conceptually simple nature of such a fascin
Externí odkaz:
https://doaj.org/article/70e0cb4b51cb4d8284aa4d40659e3270
Publikováno v:
Journal of Composite Materials. 56:2585-2598
An experimental program has been carried out for the evaluation of the delamination onset condition of various composite material systems, under the application of constant amplitude cyclic loading. Standard Double Cantilever Beam End Notch Flexure a
Autor:
Luisa Boni, Marco Bassetto, Lorenzo Niccolai, Giovanni Mengali, Alessandro A. Quarta, Christian Circi, Rocco C. Pellegrini, Enrico Cavallini
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bbb29a21c877613e09d9efb36b1615e0
https://hdl.handle.net/11573/1673484
https://hdl.handle.net/11573/1673484
Publikováno v:
Acta Astronautica. 179:99-104
We address the heliocentric in-orbit repositioning problem of an E-sail-based spacecraft that covers a circular parking orbit of given radius, with the assumption that the propulsive acceleration is directed along the Sun-spacecraft line. According t
Publikováno v:
Acta Astronautica. 175:510-516
The propulsive characteristics of an Electric Solar Wind Sail are usually evaluated using a simplified model in which all the sail tethers are coplanar and form a sort of rigid disk. However, the three-dimensional arrangement of the tethers is fundam
Autor:
Marco Bassetto, Lorenzo Niccolai, Luisa Boni, Giovanni Mengali, Alessandro A. Quarta, Christian Circi, Simone Pizzurro, Marco Pizzarelli, Rocco C. Pellegrini, Enrico Cavallini
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::436836de1d5f1ddfcd4d319f2c279966
https://hdl.handle.net/11573/1673479
https://hdl.handle.net/11573/1673479
Publikováno v:
Aerospace Science and Technology. 130:107920
Publikováno v:
Composites Part B: Engineering. 153:97-107
An experimental program has been carried out at the Department of Civil and Industrial Engineering of the University of Pisa, in collaboration with Leonardo Helicopter Division (formerly AgustaWestland), for the evaluation of the interlaminar fractur
Publikováno v:
Engineering Fracture Mechanics. 254:107918
The study investigates fatigue growth and shape evolution of a corner crack in a pin-loaded hole by means of three-dimensional FE analyses. The constraint factor/plasticity-induced crack closure strategy was tuned to reproduce experimentally measured
Publikováno v:
ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing ISBN: 9783030215026
An experimental program has been carried out for the evaluation of the influence of the split sleeve expansion process on the fatigue crack growth in 2024-T351 aluminium alloy specimens. In previous ICAF Symposia, some information has been already gi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::deed1843379c3d1d581a32643e7de487
http://hdl.handle.net/11568/998398
http://hdl.handle.net/11568/998398