DIRE - Dactyl-Ida Rendezvous Experiment

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Please use this identifier to cite or link to this item: http://hdl.handle.net/1853/8030

Title: DIRE - Dactyl-Ida Rendezvous Experiment
Author: Pengelly, Stan ; Adams, J. Brian ; Platt, Donald
Abstract: The purpose of this paper is to discuss, at the system level, a theoretical spacecraft and mission named DIRE (Dactyl-Ida Rendezvous Experiment). The spacecraft will travel to the asteroid pair Dactyl and Ida, which is approximately 3 AU from the Sun, to achieve the following mission objectives: • Measure the magnetic fields around the asteroid pair and each object individually. • Take multispectral images at various altitudes to determine surface regolith composition and distribution. • Using ground penetrating radar, attempt to discern the hidden structure of Ida and Dactyl and answer this question: are asteroids actually many rocks loosely coalesced into a single body and held together by gravity, rather than a huge monolith? • Descend autonomously to each asteroid and retrieve samples of regolith, using micropropulsion systems. Analysis of regolith will then be performed with on board systems. • Near the end of the mission launch a ground-penetrating explosive into Dactyl in an attempt to split into its subparts. The purpose here is to develop a technique for neutralizing a possible Earth damaging asteroid by separating it into smaller, less dangerous objects. DIRE will then make radar measurements of the ensuing asteroid breakup and determine if and how the asteroid re-coalesces. • Get a first ever look at material from within an asteroid, after the explosive splits Dactyl. This mission uses features of previous spacecraft missions and adds a never before attempted explosive penetrator to probe deeply and precisely into an asteroid. Thus, this mission will add to deep space object science and perhaps provide a way for mankind to defend itself against them.
Description: This conference features the work of authors from: Georgia Tech’s Space Systems Design Lab, Aerospace Systems Design Lab, School of Aerospace Engineering, Georgia Tech Research Institute; NASA’s Jet Propulsion Laboratory, Marshall Space Flight Center, Goddard Space Flight Center, Langley Research Center; and other aerospace industry and academic institutions
Type: Presentation
URI: http://hdl.handle.net/1853/8030
Date: 2005-11-10
Contributor: General Dynamics Corporation
Micro Aerospace Solutions
Georgia Institute of Technology. Space Systems Design Lab
Relation: SSEC05 Session C;GT-SSEC.C.4
Publisher: Georgia Institute of Technology
Subject: Deep space object science
Defense against Earth damaging asteroids
Explosive penetrators
Ground penetrating radar
Micropropulsion systems
Multispectral images
Probes
Radar measurements
Sample retrieval from asteroids
Theoretical spacecraft

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