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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.

  • p. 7 …sign, the total energy and momentum of the combined system remains zero for all times, leaving…
  • p. 8 …of special relativity, being the expression of a Minkowskian space-time structure, there is an older…
  • p. 10 …With lxl = (1/r, where OJ= 2tr/T, with T the time of revolution, and r…
  • p. 11 …time before their fields propagating with the velocity of light would reach the earth. Adding the…
  • p. 16 …Even though its time-averaged velocity is always less than the velocity of light, this means…
  • p. 18 …0~ m· =12r ~6X1Q-13g, ( 45) larger by a factor 3.6x10 11 times the mass…
  • p. 22 …by saying that the zero-point vacuum energy "generates" the Minkowski space-time. 7. Dynamic Interpretation…
  • p. 23 …the rod is /, and if the rod rests in the distinguished reference system, the time needed…
  • p. 24 …c -v Slll-1// -VCOSlf/ (67) with the time t' for a to and fro signal…
  • p. 25 …If tR is the absolute reflection time of the light signal at clock B, one has…
  • p. 26 …using a rod to measure the distance and the time it takes a light signal in…
  • p. 34 …The time needed to bring back the universe to its original low entropy state, is the…
  • p. 37 …times more dense than water 16. Suppose that in the center of the moon the accumulation…
  • p. 38 …the heat diffusion equation given by (109) where Xis the heat diffusion coefficient, the diffusion time…
  • p. 39 UNCLASSIFIED/ ,'P81l 81'1'11!111it 1!1!11!! 811LY The time needed for the liquid…
  • p. 42 …This means that a small, continuous removal of the heat through the injection and circulation of…
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

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Report, from the dia collection. The PDF is mirrored here; the original link is under it. 43 pages are in the text index: search them above, or from the library's search.