Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Simone Ciaralli"'
Autor:
André Nyberg Borrfors, Dan J. Harding, Jonas Weissenreider, Simone Ciaralli, Ashley Hallock, Tore Brinck
The aromatic hydrocarbons (AHs) fluorobenzene, naphthalene, and 1fluoronaphthalene are introduced as promising alternatives to xenon as propellant for in-space electric propulsion (EP). These storable molecules have similar mass, lower cost, and lowe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f2324dc8a2629adf440bc1e2b30a153e
https://doi.org/10.21203/rs.3.rs-2666479/v1
https://doi.org/10.21203/rs.3.rs-2666479/v1
Autor:
Sergio Castellano, Daniele Seglie, Andrea Gazzola, Luca Racca, Simone Ciaralli, Olivier Friard
Publikováno v:
Behavioral Ecology and Sociobiology. 76
Abstract We studied how individuals modify their behavior in response to inter- and intraspecific competitors and how these changes affected the pattern of variation between populations and species. As study models, we used tadpoles of two brown frog
Publikováno v:
Aerospace Science and Technology. 47:291-298
This paper describes the design and testing of the engineering model of a pulsed plasma thruster for Cubesat applications (PPTCUP-EM). It has been developed by Mars Space Ltd, Clyde Space Ltd and the University of Southampton with the main aim of inc
Publikováno v:
IEEE Transactions on Plasma Science. 43:218-225
In this paper, the design and performances of apulsed plasma thruster (PPT) for nanosatellite applications willbe presented. The breadboard model PPT presented in this paperwill be a part of six PPTs propulsion system designed to provideattitude and
Pulsed Plasma Thruster for Cubesat Propulsion (PPTCUP) is an ablative pulsed plasma thruster designed with the aim of providing translational and orbital control to Cubesat platforms. The qualification model presented in this paper has been developed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3d580c4ec3da8bc1e85556ca75f604c0
https://eprints.soton.ac.uk/383092/
https://eprints.soton.ac.uk/383092/
Publikováno v:
Measurement Science and Technology. 24:115003
This paper describes the design and testing of a direct torsional impulsive thrust balance. The design philosophy allows the balance to measure impulse bits (Ibit) in the range of 20?120??N?s typical of pulsed plasma thrusters (PPTs) for pico- and na