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Experimental Results of Schlicher's Thrusting AntennaExperiments were conducted to test the claims by Rex L. Schlicher, et al., (Patent 5,142,86 1) that a certain antenna geometry produces thrust greatly exceeding radiation reaction, when driven by repetitive, fast rise, and relatively slower decay current pulses. In order to test this hypothesis, the antenna was suspended by strings as a 3 in pendulum. Current pulses were fed to the antenna along the suspension path by a very flexible coaxial line constructed from loudspeaker cable and copper braid sheath. When driving the antenna via this cabling, our pulser was capable of sustaining 1200 A pulses at a rate of 30 per second up to a minute. In this way, bursts of pulses could be delivered in synch with the pendulum period in order to build up any motion. However, when using a laser beam passing through a lens attached to the antenna to amplify linear displacement by a factor of at least 25, no correlated motion of the beam spot could be detected on a distant wall. We conclude, in agreement with the momentum theorem of classical electromagnetic theory, that any thrust produced is far below practically useful levels. Hence, within classical electrodynamics, there is little hope of detecting any low level motion that cannot be explained by interactions with surrounding structural steel and the Earth's magnetic field.
Document ID
20020009088
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Fralick, Gustave C.
(NASA Glenn Research Center Cleveland, OH United States)
Niedra, Janis M.
(QSS Group, Inc. Brook Park, OH United States)
Date Acquired
September 7, 2013
Publication Date
November 1, 2001
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2001-211207
AIAA Paper 2001-3657
NAS 1.15:211207
E-13058
Meeting Information
Meeting: 37th Joint Propulsion Conference and Exhibit
Location: Salt Lake City, UT
Country: United States
Start Date: July 8, 2001
End Date: July 11, 2001
Sponsors: American Society of Mechanical Engineers, American Inst. of Chemical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 713-74-70
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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