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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…
UNCLASSIFIED/ /F&~ 8FFHiil.«1k 1!181! &••kY
- K"' 1.5.t
• Electron Beam:
- Photocathode injector creates picosecond electron pulses at 7 MeV. t
- Superconducting accelerator increases electron energy to 100 MeV.
- Peak current: 1100 A.
- Average current: 0.5 A.
- Length: 0.1 mm.
- Radius: 0.1 mm.
- Electron beam recirculated for energy recovery.
• Optical resonator based on short Rayleigh length optical mode (see Figure 32):
- Cavity length (resonator mirror separation distance), 5: 16 m.
- Optical waist (natural mode width), wo: 0.1 mm.
- Mirror radius of curvature, w: 2.6 cm.
Rayleigh length, zo: 2 cm.
• Optical (Laser Beam) Output:
- Power: 2 MW.
- Wavelength, /,: 1 μm (tunable by controlling electron beam, undulator and
resonator properties).
• Short Rayleigh length§ (SRL) optical mode gives several advantages:
Reduces optical intensity on resonator mirrors to avoid mirror damage.
- Single optical wavefront is amplified giving excellent beam quality.
- FEL interaction is altered with SRL mode.
- SRL intensifies interaction at mode focus.
■ Rapidly changing optical amplitude and phase.
- SRL accelerates electron bunching and energy extraction
■ Electrons interact with optical radiation field along undulator.
■ Electrons "see" intense optical electric field at mode focus.
■ Electrons "see" rapidly changing optical radiation phase at mode focus.
• Natural mode width/optical waist (for 5 ~ meters & laser beam f. ~ microns) is
millimeters.
• High-power lasers typically run in multiple transverse modes; however:
- High-power FEL requires short Rayleigh length and small optical waist.
- High-power FEL amplifies single mode without damage to gain medium (a
vacuum).
• FEL efficiency increases as Rayleigh length decreases.
• For megawatt-class FEL system, high operating current plus active mirror
alignment system acts to stabilize optical mode against Naval warship vibrations,
'K"' eB,rn,f,,.,nol2rcmC, where e is the electron charge, B,.,, is the root-mean-square magnetic field strength, /,,no
is the undulator period, mis the electron mass, and c is the speed of light.
'MeV "' Mega-electron Volt.
•sRL = distance for the area of the beam waist to double.
61
UNCLASSIFIED/ }FQA: QFFIQIOk WEliii Qllk>f

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