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Defense Intelligence Reference Document Negative Mass Propulsion

Defense Intelligence Agency · 43 pages · text from the file's own layer

This Defense Intelligence Reference Document from the Defense Intelligence Agency is dated 3 January 2011. It was produced under the Advanced Aerospace Weapon System Applications (AAWSA) Program as part of a series of advanced technology reports. The report asks whether negative mass exists and whether it could be used for propulsion. It concludes that one route might be an ultra-light form of matter that could have gathered at the Moon's center. Reaching it would take a tunnel dug with thermonuclear shape charges.

,. e H ,urp = -- ffr-
hc
e ,
i5R. (99)
As noted by Aharonov and Bohm [11], there is a phase shift for r > R, even though for
r > R, H = 0 (because for r > R, curl A= 0).
Expressing A by (84) through v, the hypothetical circular aether velocity, one has
e
v =---Hr
~' 2mc r R. (100)
One sees that inside the coil the velocity profile is the same as in a rotating frame of
reference, having outside the coil the form of potential vortex. If expressed in terms of
the aether velocity the phase shift becomes
(101)
the same as (97) for the vector potential created by a gravitational field, and hence the
same as in the Sagnac experiment and neutron interference experiment. But for the
magnetic vector potential the aether velocity can easily become much larger than in
any rotating platform experiment. According to (102), the velocity reaches a maximum
at r = R, where it is
Iv"'" I eHR
c 2rnc 2 •
(102)
For electrons this is lvma, 1/c = 3x l0-4 HR, where His measured in Gauss. For H = 104 G,
this would mean that vmax 2 c for R > 0.3 cm. If this would be same aether velocity felt
on a rotating platform, it would lead to an enormous centrifugal and Coriolis field inside
the coil, obviously not observed.
28
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Report, from the dia collection. The PDF is mirrored here; the original link is above. 43 pages are in the text index: search them above, or from the library's search.