Deflection of near-Earth asteroids by kinetic energy impacts from retrograde objects
McInnes, C.R. (2004) Deflection of near-Earth asteroids by kinetic energy impacts from retrograde objects. Planetary and Space Science, 52 (7). pp. 587-590. ISSN 0032-0633 (http://dx.doi.org/10.1016/j.pss.2003.12.010)
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Previous studies of non-nuclear diversion of near Earth asteroids have largely ignored the use of pure kinetic energy impacts, partly due to apparent limits on impact speeds of 10-15 km s−1. Here, I will consider the use of a near-term solar sail to deliver an inert projectile onto a retrograde solar orbit, thus raising impact speeds to at least 60 km s−1. Such high-energy orbits increase the energy liberated during impact by a factor of 40 or more, while reducing the required projectile mass by at least 95%. This considerable reduction in projectile mass allows kilometre-sized asteroids to be diverted with current launch vehicles, near-term technologies and at a cost comparable to a modest deep space mission.
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Item type: Article ID code: 5031 Dates: DateEvent2004PublishedSubjects: Technology > Mechanical engineering and machinery
Technology > Motor vehicles. Aeronautics. AstronauticsDepartment: Faculty of Engineering > Mechanical and Aerospace Engineering Depositing user: Strathprints Administrator Date deposited: 20 Dec 2007 Last modified: 11 Nov 2024 08:42 URI: https://strathprints.strath.ac.uk/id/eprint/5031