Title :
Deep Impact, the mission
Author :
Muirhead, Brian K.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Abstract :
This paper discusses the Deep Impact (DI) mission (the 8th Discovery Mission) objectives and potential discoveries derived from impacting a comet nucleus at ten times the speed of a bullet and simultaneously observing the results of that impact. The scientific return from this mission centers on 13 minutes of critical operations while flying through a comet´s coma on July 4, 2005. A detailed mission and spacecraft description is provided including science instruments. The overall implementation approach is discussed, including the special shared development and operations responsibilities among JPL, Ball Aerospace and University of Maryland. This paper also discusses the unique challenges of this mission especially the unknowns and potential hazards of flying deep into the comet environment (e.g. dust, surface topography, structure and composition). The design for robustness in the face of significant unknowns is discussed including autonomous navigation to track and hit a target, at a relative speed of 10 km/s.
Keywords :
aerospace control; aerospace instrumentation; cometary nuclei; dust; impact (mechanical); navigation; risk management; space research; space vehicles; surface topography; target tracking; 10 km/s; 13 min; DI mission; Deep Impact Discovery mission; autonomous navigation; comet coma fly-through critical operation time; comet environment unknowns/potential hazards; comet structure/composition; design for robustness; dust; mission objectives/potential discoveries; risk management; spacecraft comet nucleus impact observations; spacecraft science instruments description; surface topography; target relative speed; target tracking; Aircraft manufacture; Composite materials; Hazards; Instruments; Laboratories; Project management; Propulsion; Space technology; Space vehicles; Surface topography;
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
DOI :
10.1109/AERO.2002.1036835