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Non-Rocket Missile Rope LauncherThe method, installation, and estimation for delivering payload and missiles into outer space are presented. This method uses, in general, the engines and straight or closed-loop cables disposed on a planet surface. The installation consists of a space apparatus, power drive stations located along trajectory of the apparatus, the cables connected to the apparatus and to the power stations, a system for suspending the cable, and disconnected device. The drive stations accelerate the apparatus up to hypersonic speed. The estimations and computations show the possibility of making these projects a reality in a short period of time (see attached project: launcher for missiles and loads). The launch will be very cheap $1-$2 per LB. We need only light strong cable, which can be made from artificial fibers, whiskers, nanotubes, which exist in industry and scientific laboratories.
Document ID
20030018907
Acquisition Source
Headquarters
Document Type
Preprint (Draft being sent to journal)
Authors
Bolonkin, Alexander
(National Academy of Sciences - National Research Council Elgin AFB, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
IAC-02-S.P.14
Meeting Information
Meeting: 53rd International Astronautical Congress: The World Space Congress
Location: Houston, TX
Country: United States
Start Date: October 10, 2002
End Date: October 19, 2002
Distribution Limits
Public
Copyright
Public Use Permitted.
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