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Energy Considerations of Hypothetical Space DrivesThe energy requirements of hypothetical, propellant-less space drives are compared to rockets. This serves to provide introductory estimates for potential benefits and to suggest analytical approaches for further study. A "space drive" is defined as an idealized form of propulsion that converts stored potential energy directly into kinetic energy using only the interactions between the spacecraft and its surrounding space. For Earth-to-orbit, the space drive uses 3.7 times less energy. For deep space travel, energy is proportional to the square of delta-v, whereas rocket energy scales exponentially. This has the effect of rendering a space drive 150-orders-of-magnitude better than a 17,000-s Specific Impulse rocket for sending a modest 5000 kg probe to traverse 5 ly in 50 years. Indefinite levitation, which is impossible for a rocket, could conceivably require 62 MJ/kg for a space drive. Assumption sensitivities and further analysis options are offered to guide further inquires.
Document ID
20070031912
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Millis, Marc G.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 23, 2013
Publication Date
July 9, 2007
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2007-5594
E-16239
Report Number: AIAA Paper 2007-5594
Report Number: E-16239
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Cincinnati, OH
Country: United States
Start Date: July 9, 2007
End Date: July 12, 2007
Sponsors: American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 732759.03.01.01.08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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