Documents / Report

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.

  • p. 43 …873 (2002). 16. S. Badiei, P.U. Anderson, L. Holmlid, International Journal of Mass Spectroscopy 282…
UNCLASSIFIED/ ,'P81l 81'1'11!111it 1!1!11!! 811LY
The time needed for the liquid metal to pass through a ~ 20 m thick layer is then ~ 2 x
103 seconds~ 1 hour. The specific heat per unit volume of the coolant is pc, ~ 3 x 107
erg/cm 3K, and for T = 3 x 103 Kone has pcJ ~ 10 11 erg/cm 3 .
The heat per unit volume which has to be removed from the crushed rocks is of the
order p, where p is the rock pressure. In the center of the moon where p = 5 x 1010
dyn/cm 2 , this energy is 5 x 10 10 erg/cm 3 . It thus follows that the volume of the liquid
coolant must be about 1/2 of the rock volume to be cooled. For a rock volume of (20
cm) 3 ~ 104 m 3 , a coolant volume of about 5 x 10 3 cm 3 would be needed. The same
coolant can be used many times over after the heat is removed from it, which could be
done on the surface of the moon by radiation or perhaps better by heat exchangers
transferring the heat to lunar sand. Without a thick layer of shattered rocks surrounding
the tunnel, the pressure acting on the tunnel wall would be large, in particular in the
center of the moon. Because of friction between particles of the shattered rock, large
shear stresses can be sustained changing the pressure distribution in the rock and
reducing the pressure gradient and hence the pressure on the tunnel wall.
A more detailed calculation [15] for the pressure distribution in the shattered rock
tunnel wall gives
(113)
where ro is the radius of the tunnel.
Integrating eqn (108) one obtains for the pressure distribution in the moon
(114)
for which one can also write
p(r) ~ P,,,,, (,-(; )'J. (115)
35
UNCLASSIFIED/ ,'1'81l 81'1'11!111it 1!1!11!! 811LY

Not linked to a story yet.

About this file

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.