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AAWSAP DIRD, Aneutronic Fusion Propulsion II, November 2010

U.S. Department of War · 2010-11-01 · 36 pages · text from the file's own layer

This Defense Intelligence Reference Document, dated 1 November 2010, was prepared by the Defense Intelligence Agency's Defense Warning Office under the Advanced Aerospace Weapons System Applications program. It reviews fusion plasma physics, confinement methods and propulsion concepts that use aneutronic fusion fuels such as hydrogen and boron-11. It concludes that pulsed DPF or IEC thrusters may replace satellite ion thrusters in the near term. It also finds that aneutronic fusion propulsion will not be practical beyond the solar system without breakthrough propulsion physics.

From the source: Release of 2026-09-18 Incident: 11/1/10, 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 revisits aneutronic fusion propulsion in a more systems-oriented manner, arguing that fusion concepts using low-neutron fuels such as proton-boron or helium-3 could become attractive for space propulsion because they reduce shielding burdens and may support direct conversion of charged-particle energy into thrust or onboard power. The report reviews the relevant fusion plasma physics and focuses on several candidate confinement approaches, then connects those concepts to possible applications in near-space, orbital, and interplanetary propulsion. It presents the most plausible nearer-term use as very high-power electric or plasma propulsion for satellites and deep-space missions rather than atmospheric flight or interstellar travel, while emphasizing that major obstacles remain in ignition, sustained confinement, system mass, power handling, fuel storage, launch integration, and end-to-end engineering.

UNCLASSIFIED// FOR OFFICIAL l:ISI: 8HLY
The perennial challenge for developing such a device into a power reactor is the feat of
manufacturing and compressing 10 such 1-mm DT fuel pellets per second. One
significant problem is maintaining equal pressure on the pellets repeatedly to permit
energy production.
ELECTROSTATIC CONFINEMENT
This simple method of confinement is composed of concentric spheres (or sometimes
cylinders) acting as anode and cathode in a vacuum known as a Farnsworth-Hirsch
Fusor or, more commonly, Inertial Electrostatic Confinement (IEC). As shown in Figure
5, the inner sphere (cathode) is not solid, but rather is composed of a wire grid. Ions
entering the vacuum chamber between the anode and cathode are accelerated through
a large potential difference toward the cathode. Passing through the cathode, the ions
collide in the central region, with a small portion of the plasma population undergoing
fusion. 1• 2, 3 However, using this simple setup, it has been argued that net energy
production is not viable for anything other than deuterium-tritium fusion, in part
because the fusion-collision cross section is several orders of magnitude smaller than
the Coulomb-collision cross section. 4 An additional difficulty is that some of the plasma
interacts directly with the cathode, contaminating the plasma with heavy sputtered ions.
A method for mitigating this problem is to eliminate the cathode grid and instead use
magnetic (and electrostatic) fields to create a virtual cathode composed of electrons.
Such devices include the Polywell 5 and the Penning trap. 6 One such Penning trap design
developed at Los Alamos injects electrons into the central region in such a manner as to
produce a harmonic oscillator potential. Called a Periodically Oscillating Plasma Sphere
(POPS), ions in this chamber then also undergo harmonic oscillations and can become
phase-locked with the use of an externally applied radiofrequency electric field.71 8 This
allows the ions to reach very high densities and temperatures as they collide at the
center of the chamber. This promising design eliminates any power loss due to Coulomb
collisions and substantially increases the efficiency of fusion-power generation.
Figure S. IEC Fusor and Polywell Confinement Configurations
UNCLASSIFIED//FOR OSSICI0~ Ui&i &NL¥
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Official release, from the pursue collection. The PDF is mirrored here; the original link is above. 36 pages are in the text index: search them above, or from the library's search.