The SIROCO Asteroid Deflection Demonstrator

Bombardelli, Claudio ORCID:, Urrutxua, Hodei, Gálvez, Andrés and Carnelli, Ian (2012). The SIROCO Asteroid Deflection Demonstrator. In: "22nd AAS/AIAA Space Flight Mechanics Meeting", 29/01/2012 - 02/02/2012, Charleston, South Carolina, USA. ISBN 978-0-87703-581-7. pp. 1883-1892.


Title: The SIROCO Asteroid Deflection Demonstrator
Item Type: Presentation at Congress or Conference (Article)
Event Title: 22nd AAS/AIAA Space Flight Mechanics Meeting
Event Dates: 29/01/2012 - 02/02/2012
Event Location: Charleston, South Carolina, USA
Date: 2012
ISBN: 978-0-87703-581-7
Volume: 143
Faculty: E.T.S.I. Aeronáuticos (UPM)
Department: Física Aplicada a la Ingeniería Aeronáutica [hasta 2014]
Creative Commons Licenses: Recognition - No derivative works - Non commercial

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There is evidence of past Near-Earth-Objects (NEOs) impacts on Earth and several studies indicating that even relatively small objects are capable of causing large local damage, either directly or in combination with other phenomena, e.g. tsunamis. This paper describes a space mission concept to demonstrate some of the key technologies to rendezvous with an asteroid and accurately measure its trajectory during and after a deflection maneuver. The mission, called SIROCO, makes use of the recently proposed ion beam shepherd (IBS) concept where a stream of accelerated plasma ions is directed against the surface of a small NEO resulting in a net transmitted deflection force. We show that by carefully selecting the target NEO a measurable deflection can be obtained in a few weeks of continuous thrust with a small spacecraft and state of the art electric propulsion hardware.

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Item ID: 22875
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Deposited by: Memoria Investigacion
Deposited on: 25 Apr 2014 17:20
Last Modified: 15 Feb 2023 07:55
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