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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 …Laser Lightcraft Weapon Mission Selection Study .................................. 27 Chapter 4: Summary of Multi-Megawatt Laser Study for…
  • p. 5 …Many of these missions require numerous small spacecraft in a constellation or "swarm." These include orbital…
  • p. 7 …Simple, effective methods of thermal control are essential to keep the nanosat operational during extreme temperature…
  • p. 8 …GUIDANCE, NAVIGATION AND CONTROL Guidance Navigation and Control (GN&C) subsystem key technologies and concepts have…
  • p. 13 …Streamlined testing is needed for up to 100 or 1000 nanosats per mission. Performing a complete…
  • p. 14 …the mission lifetime. The remote agents achieve this goal by monitoring and appropriately controlling nanosat subsystems…
  • p. 33 …Thus, the selected Lightcraft missions are launch vehicle missions involving 29 UNCLASSIFIED//F&R 8FFI&I…
  • p. 40 …An air-launched Lightcraft launch vehicle mission, involving the transport of lasers and Lightcraft on medium…
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- 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
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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.