Conceptual Design of a Hypervelocity Asteroid Intercept Vehicle (HAIV) and its Flight Validation Mission

A. Pitz, B. Kaplinger, G. Vardaxis, T. Winkler, B. Wie
<span title="2012-08-13">2012</span> <i title="American Institute of Aeronautics and Astronautics"> AIAA/AAS Astrodynamics Specialist Conference </i> &nbsp; <span class="release-stage">unpublished</span>
An intercept mission with nuclear explosives is the only practical mitigation option against the most probable impact threat of near-Earth objects (NEOs) with a short warning time (e.g., much less than 10 years). The existing penetrated subsurface nuclear explosion technology limits the intercept velocity to less than approximately 300 m/s. Consequently, an innovative concept of blending a hypervelocity kinetic impactor with a subsurface nuclear explosion has been developed for optimal
more &raquo; ... on, fragmentation, and dispersion of the target NEO. A proposed HAIV (hypervelocity asteroid intercept vehicle) consists of a kinetic-impact leader spacecraft and a follower spacecraft carrying nuclear explosives. This paper describes the conceptual development and design of a baseline HAIV system and its flight validation mission architecture for three mission cost classifications (e.g., $500M, $1B, and $1.5B).
<span class="external-identifiers"> <a target="_blank" rel="external noopener noreferrer" href="">doi:10.2514/6.2012-4873</a> <a target="_blank" rel="external noopener" href="">fatcat:dx6amvki4fc7llttud3l7ict3q</a> </span>
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