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Defense Intelligence Reference Document Aneutronic Fusion Propulsion (2)

Defense Intelligence Agency · 36 pages · text from the file's own layer

This Defense Intelligence Agency reference document, dated 1 November 2010, is one of a series of advanced technology reports produced in FY 2010 under the Advanced Aerospace Weapons System Applications (AAWSA) Program. It covers fusion plasma physics, confinement methods, and propulsion concepts that use aneutronic fuels such as hydrogen and boron-11. It concludes that such thrusters may soon replace satellite ion thrusters. It also finds that they will not be practical beyond the solar system without breakthrough propulsion physics.

  • p. 4 …Colliding Beam Fusion Reactor .............................................................. 12 Figure 10. DPF Thruster System With Direct Conversion ...................................... 12 Figure 11…
  • p. 5 …for confinement pulsed power and ion fuel beam accelerators. V UNCLASSIFIED/F8R 8FFICJ0P !IEE ANI Y
  • p. 6 …Magnetic confinement devices utilized the IEC method with imploding layers of lithium or applying intense beams…
  • p. 12 …using high-energy lasers or using particle beams ( electrons or ions). The vast majority of ICF…
  • p. 14 …can be substituted for lasers or particle beams to compress the target. A lower implosion velocity…
  • p. 16 …Optimization of this conceptual design using the FRC plasma confinement using colliding beams has led to…
  • p. 17 …Colliding Beam Fusion Reactor Cheung et al. 2004 Dense Plasma Focus Reactors The Dense Plasma Focus…
  • p. 18 Magnetic Expansion Chamber UNCLASSIFIED//F81il 8FFI1il.t.k Wfili 8Hklf BURN CHAMBER I Fuel Beam I…
  • p. 19 …Such designs then accelerate and focus ions into a beam, using an electrostatic potential, with a…
  • p. 22 …The addition of a 150-kWe ion beam for heating a (p, 11 B) plasma close…
  • p. 26 …The HEDLPP program covers the following areas: • Radiative hydrodynamics. • Laser-plasma and beam-plasma interaction. • Fusion…
  • p. 28 …Both Lawrenceville Plasma Physics (which uses DPF, dense plasma focus, confinement) and TriApha (which uses beam…
  • p. 29 …Current: $11M (p,"B) Needed:$1OOM TriAlpha Beam-Heated Field (p,"B) Current : $SOM Reversed Conf…
  • p. 31 …Lightweight For particle beam !EC, CBFR Most experiments are particle injection, energy currently ground oriented - accelerators…
  • p. 33 …production needs 10 he ren-cled ,ia beam direct conYersinn "ith electron escape 01· ndinaed back…
  • p. 35 …This could be extended to the very high-power domain of beam-assisted FRC for manned…
  • p. 36 …Rahman, and J.O'Toole, "Colliding Beam Fusion Reactor Space Propulsion System," Space Technology and Applications…
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Chapter 7: Conclusions
Much of the groundwork (literally) for aneutronic fusion propulsion has been
accomplished, including conducting fusion experiments, development of design
concepts, and the analysis of applications to aerospace propulsion. Transitioning these
concepts to space is an immense challenge given the large mass, power requirements,
and support engineering for power conversion, energy recovery, and fuel storage. This
transition, however, may depend upon the success of the developments of privately
funded ventures attempting to develop terrestrial power. Notwithstanding such
developments, their application for both military and space or near-space applications
requires a much lower threshold for return on investment than terrestrial power.
Pulsed-powered DPF or IEC aneutronic fusion thrusters may have near-term
applications to replace current satellite ion thrusters. This could be extended to the very
high-power domain of beam-assisted FRC for manned interplanetary flight. The near-
space domain will require major improvements in technology to reduce system mass
since the size enters the MW range. The application to the aircraft domain will require
further developments in technology to reduce system mass and/or the use of DT fuels,
which present other potential safety issues. Aneutronic fusion propulsion will not be
practical beyond the solar system unless breakthrough propulsion physics is developed
that can assist the flight to the next stellar system where fusion thrusters can then be
used.
Whether it is reducing rows and rows of capacitor banks to pulse generators, shrinking
immense superconducting magnets to a more compact and lightweight geometry, or
engineering integrated fusion propulsion systems to fit onto a booster rocket, the
physicists who pioneered much of the reactor and propulsion technology must now
work side-by-side with the space systems companies to explore viable propulsion
systems from implementation to on-orbit maintenance and attitude control. The future
needs to be focused more on science and engineering and less on science fiction.
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Report, from the dia collection. The PDF is mirrored here; the original link is under it. 36 pages are in the text index: search them above, or from the library's search.