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Multi-Mission Space Exploration Vehicle Concept Simulation of Operations in Proximity to a Near Earth ObjectThis paper details a project to simulate the dynamics of a proposed Multi-Mission Space Exploration Vehicle (MMSEV), and modeling the control of this spacecraft. A potential mission of the MMSEV would be to collect samples from a Near-Earth Object (NEO), a mission which would require the spacecraft to be able to navigate to an orbit keeping it stationary over an area of a spinning asteroid while a robotic arm interacts with the surface.
Document ID
20150006634
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
Authors
Kline, Heather
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
April 24, 2015
Publication Date
August 15, 2011
Subject Category
Ground Support Systems And Facilities (Space)
Lunar And Planetary Science And Exploration
Astronautics (General)
Distribution Limits
Public
Copyright
Other
Keywords
Near Earth Object (NEO)
reaction wheels
thrusters
asteriod

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