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AAWSAP DIRD, Advanced Nuclear Propulsion for Manned Deep Space Missions, March 2010

U.S. Department of War · 2010-03-11 · 37 pages · text from the file's own layer

This Defense Intelligence Reference Document is dated 11 March 2010. It was prepared by the Defense Intelligence Agency's Defense Warning Office as part of the Advanced Aerospace Weapon System Applications program. It is a technical paper arguing that spacecraft driven by deuterium thermonuclear reactions could be built with current science and could reach the outer solar system. It covers magnetic insulation, ignition by proton beams, a Super Marx generator and conjectured chemical superexplosives. It does not discuss any UFO sightings.

From the source:Release of 2026-09-18 Incident: 3/11/10, Las Vegas, Nevada. Released with redactions. This document is a Defense Intelligence Reference Document (DIRD), a technical reference format used by the Defense Intelligence Agency (DIA) to capture baseline knowledge on a specific topic for later analytic use. DIRDs are best understood as reference and synthesis products rather than as original research. It is one of 38 DIRDs produced under the Advanced Aerospace Weapon System Applications Program (AAWSAP) between 2009 and 2011. Because AAWSAP’s scope permitted a broad range of supporting topics, not every DIRD in the series directly concerns aerospace systems or future threat assessment. The following summary reflects the DIRD’s scope and framing at the time of writing and should not be read as implying current validation of the concepts discussed. This DIRD examines advanced nuclear propulsion for crewed deep-space travel and argues that human missions beyond the Moon would require propulsion systems with both very high thrust and very high specific impulse, which the author contends are difficult to achieve with conventional chemical, nuclear-thermal, and nuclear-electric systems. The report focuses on concepts derived from Project Orion, the discontinued General Atomics nuclear pulse propulsion study sponsored first by ARPA and later by the U.S. Air Force between 1958 and 1965, in which a spacecraft would be driven by repeated nuclear explosions. In this case, the DIRD emphasizes small non-fission-triggered fusion explosions using deuterium, magnetic mirrors, and other unconventional ignition concepts intended to avoid the inefficiencies associated with small fission devices. It presents these ideas as a possible pathway to crewed missions across the solar system, while also linking them to broader visions of long-range human expansion into space. The document is exploratory in character and depends on several unproven ignition methods, enabling technologies, and engineering assumptions. Overall, it is a theoretical examination of fusion-based pulse propulsion concepts rather than as a documentary account of a technology nearing practical realization.

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• Bombardment of a solid target with beams or by hypervelocity impact, followed by a
convergent shock wave.
BOMBARDMENT OF A SOLID TARGET WITH AN INTENSE
RELATIVISTIC ELECTRON OR ION BEAM
This possibility was considered by Kidder (Reference 20), who computes a pressure of
50 Mb, if an iron plate is bombarded with a 1-MJ - 10-MeV - 106 A relativistic electron
beam, focused down to an area of 0.1 cm 2 . Accordingly, a 2-MJ beam would produce
100 Mb. Instead of an intense relativistic electron beam, one may use an intense ion
beam. It can be produced by the same high-voltage technique, replacing the electron
beam diode by a magnetically insulated diode (Reference 21) .
Using intense ion beams has the additional benefit that the stopping of the ions in a
target is determ ined by a Bragg curve, generating the maximum pressure inside the
target, not on its surface.
HYPERVELOCITY IMPACT
A projectile with the density p :::: 20 g/cm 3 accelerated to a velocity v = 30 km/s would,
upon impact, produce a pressure of p :::: 100 Mb. The acceleration of the projectile to
these velocities can be done by a magnetic traveling wave accelerator.
BOMBARDMENT OF A SOLID TARGET WITH BEAMS OR BY
HYPERVELOCITY IMPACT, FOLLOWED BY A CONVERGENT SHOCK
WAVE
If, upon impact of either a particle beam or a projectile, the pressure is less than 100
Mb (for example, only on the order of 10 Mb) but is acting over a larger area, a tenfold
increase in the pressure over a smaller area is possible by launching a convergent
shock wave from the larger area on the surface of the target onto a smaller area inside.
According to Guderley, the rise in pressure in a convergent spherical shock wave goes
as r - 0 -9 , which means 100 Mb could be reached by a tenfold reduction in the rad ius of
the convergent shock wave.
While it is difficult to reach 30 km/s with a traveling magnetic wave accelerator, it is
easy to reach a velocity of 10 km/s with a two-stage light gas gun.
We assume an equation of state of the form pf p 0 = (n/n0 )Y . For a pressure of 100 Mb =
1 4 2 1 1 2
10 dyn/cm we may set y= 3 and p0 = 10 dyn/cm p0 be ing the Fermi pressure of, ,
a solid at the atomic number density n0 , with n being the atomic number density at the
elevated pressure p > p0 . With d = n-1/3, where d is the lattice constant, one has
(41)
Such a lowering of the inneratomic distance is sufficient for the formation of molecular
states.
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Official release, from the pursue collection. The PDF is mirrored here; the original link is above. 37 pages are in the text index: search them above, or from the library's search.