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Near Earth Object (NEO) Mitigation Options Using Exploration TechnologiesThis presentation considers the use of new launch vehicles in defense against near-Earth objects, building upon expertise in launch vehicle and spacecraft design, astronomy and planetary science and missile defense. This work also seeks to demonstrate the synergy needed between architectures for human/robotic exploration initiatives and planetary defense. Three different mitigation operations were baselined for this study--nuclear standoff explosion, kinetic interceptor, and solar collector--however, these are not the only viable options. The design and predicted performance of each of these methods is discussed and compared. It is determined that the nuclear interceptor option can deflect NEOs of smaller size (100-500 m) with 2 years or more time before impact, and larger NEOs with 5 or more years warning; kinetic interceptors may be effective for deflection of asteroids up to 300-400 m but require 8-10 years warning time; and, solar collectors may be able to deflect NEOs up to 1 km if issues pertaining to long operation can be overcome. Ares I and Ares V vehicles show sufficient performance to enable the development of a near-term categorization and mitigation architecture.
Document ID
20090008675
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Adams, Robert B.
Date Acquired
August 24, 2013
Publication Date
October 23, 2008
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
M09-2040
MSFC-2040
Report Number: M09-2040
Report Number: MSFC-2040
Meeting Information
Meeting: Asteroid Deflection Research Symposium 2008
Location: Virginia
Country: United States
Start Date: October 23, 2008
End Date: October 24, 2008
Sponsors: Iowa State Univ.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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