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Direct launch using the electric rail gunThe concept explored involves using a large single stage electric rail gun to achieve orbital velocities. Exit aerodynamics, launch package design and size, interior ballistics, system and component sizing and design concepts are treated. Technology development status and development requirements are identified and described. The expense of placing payloads in Earth orbit using conventional chemical rockets is considerable. Chemical rockets are very inefficient in converting chemical energy into payload kinetic energy. A rocket motor is relatively expensive and is usually expended on each launch. In addition specialized and expensive forms of fuel are required. Gun launching payloads directly to orbit from the Earth's surface is a possible alternative. Guns are much more energy efficient than rockets. The high capital cost of the gun installation can be recovered by reusing it over and over again. Finally, relatively inexpensive fuel and large quantities of energy are readily available to a fixed installation on the Earth's surface.
Document ID
19830026744
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barber, J. P.
(IAP Research, Inc. Dayton, OH, United States)
Date Acquired
August 11, 2013
Publication Date
February 1, 1983
Publication Information
Publication: APL The 1983 JANNAF Propulsion Meeting, Vol. 1
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
83N35015
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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