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Defense Intelligence Reference Document Laser Lightcraft Nanosatellites

Defense Intelligence Agency · 77 pages · text from the file's own layer

This Defense Intelligence Reference Document from the Defense Intelligence Agency, dated 1 November 2010, was produced under the Advanced Aerospace Weapon System Applications (AAWSA) Program. It describes nanosatellite technologies and proposes launching nanosats into orbit with laser Lightcraft propulsion. It also covers a weapon mission selection study and multi-megawatt laser options. The author recommends that the Department of Defense and NASA bring Lightcraft R&D back to the United States and restart the X-50LR flight demonstration program.

  • p. 3 …Ground/Sea-to-Space Concept ............................................................. 27 Figure 15. Air-to-Space Concept ......................................................................... 28 Figure 16. Schematic…
  • p. 31 …Ground/Sea-to-Space Concept: Appropriate rotation of a high-energy laser beam, emanating from a…
  • p. 32 …more than about 10 MW for ground/sea-based lasers, and no more than about 2…
  • p. 33 …SUMMARY AND CONCLUSIONS Ground/Sea to Space (ETO) 261 If laser propulsion can provide nearly all…
  • p. 34 UNCLASSIFIED/ /1"91t 9ffU!l"I!! l!l!il! 8111!!¥ ground, sea and air launches of…
  • p. 37 …favorable for Lightcraft than air-to- ground/sea or air-to-air missions, which are not…
  • p. 39 …to be an attractive alternative to ground/sea-based laser Lightcraft systems. In this case, airborne…
  • p. 43 …would allow detection of most air, land, sea, and space targets, as well as many "low…
  • p. 64 …The Naval Sea Systems Command's (NAVSEA) Directed Energy and Electric Weapon Systems (DE&EWS) Program…
  • p. 67 …Lightcraft nanosat or picosat from the ground, sea, or air, it will be necessary to control…
  • p. 68 …beam train suitable for ground, airborne and sea platforms. • Primary mirror which is also a deformable…
  • p. 71 …to launch laser-propelled Lightcraft from ground/sea to LEO while apertures on aircraft-mounted laser…
  • p. 72 …The entire Lightcraft launch system is comprised of a ground, sea, or airborne laser beam generator…
  • p. 73 …Launching a laser-propelled Lightcraft nanosat/picosat from the ground, sea, or air into LEO requires…
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Chapter 4: Summary of Multi-Megawatt Laser Study for
Lightcraft Propulsion Applications
SUMMARY OF LASER STUDY PERFORMED BY TEXTRON SYSTEMS
In 2002, V. Hasson (TEXTRON Systems Corporation) conducted a study of candidate
multi-megawatt laser systems for laser Lightcraft propulsion [29].
Candidate high-power/high-energy lasers identified in the study:
• Carbon Dioxide (CO2) Laser: technical issues include large wavelength and
atmospheric absorption of the laser beam.
• Carbon Monoxide (CO) Laser: technical issues include large wavelength,
atmospheric absorption of the laser beam, and toxicity of the lasing fuel (CO
gas).
• Hydrogen Fluoride (HF) or Deuterium Fluoride (DF) Laser: technical issues include
atmospheric absorption of the laser beam, corrosive lasing fuel chemicals, pulse
energy, running cost, and beam quality.
• Chemical Oxygen-Iodine Laser (COIL): technical issues include fuel chemicals,
pulse energy, and running costs.
• Bulk Slab Solid-State Laser (BSSSL): technical issues include cost, average
power, and run duration.
The first four gas dynamic and chemical laser candidates have already demonstrated
megawatt-class average beam output power. The study then reviewed the
development, testing and operational legacy of the first candidate laser technology,
which included a review of the various system architectures that use other gas mixtures
combined with CO2. The study recommended a new design for a 10 MW (beam output
power) electron gun-driven CO2/gas mixture laser because this technology does not
require additional R&D and can be implemented now. The other gases selected for the
lasing fuel are N2 and H2, which, in combination with CO2, offer superior performance
over systems using helium.
However, very recent technologically disruptive innovations led to the 10-fold increase
in the beam output power of bulk slab SSLs and their newly emergent solid-state
cousin, called high-power fiber lasers, which has made these devices more competitive
with high-power chemical and gas dynamic lasers on the basis of average beam power,
peak beam power, electrical wall plug and optical efficiencies, cost, complexity, mass,
and size. Free-electron lasers are another class of laser technology that was not
reviewed by Hasson, but recent technological innovations are accelerating their
development to the point where their present average beam output power of 20 kW will
be increased to 100 kW or higher within the next 12 to 24 months following the
publication of this report. The output beams of several of these laser devices can be
optically combined to produce a single beam with megawatt-class average output
power. It is for this reason that we will summarize their technology in Summary of
Emergent High-Power Solid-State and Free-Electron Laser Technologies section.
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Report, from the dia collection. The PDF is mirrored here; the original link is under it. 77 pages are in the text index: search them above, or from the library's search.