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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. 12 …The capability of uploading flight software changes, as well as sending a master reset if necessary…
  • p. 47 …power, beam combining concept. • Power oscillator or master oscillator-power amplifier (MOPA) design. • Unstable optical resonator…
  • p. 50 …and cold-flow assessment are 29: • 4 Master Oscillators~ $20.0 Million. • Cold-Flow Subscale Upgrades…
  • p. 54 …wavelength tunability. • Variety of power oscillator or master oscillator-power amplifier (MOPA) designs. • Scalability of beam…
  • p. 57 …optical efficiencies. • Variety of power oscillator or master oscillator-power amplifier designs (see Figure 22). • Scalability…
  • p. 58 UNCLASSIFIED/ ,sralil &FFI&Itltl H:81! 8HLY Master Oscillator, Power Amplifier (MOPA) Fiber coupled pump modules…
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Figure 34. HEL Beam Pointer/Tracker ................................................................... 65
Figure 35. Basic Shared Aperture Beam Control System ......................................... 66
Figure 36. HEL Adaptive Optics System ................................................................ 67
Tables
Table 1. Laser Lightcraft Model Cost Summary ...................................................... 25
Table 2. Performance and Estimated Weights for a Hybrid Rocket and Lightcraft ........ 30
Table 3. Estimated Costs for Hybrid Rocket and Lightcraft Launch Vehicles for ETO
Flight .............................................................................................................. 32
Table 4. Influence of Target Velocity and Intercept Angle on Impact Energy and
Required Mass .................................................................................................. 33
Table 5. Influence of Lightcraft and Target Velocity on Impact Energy and Required
Mass ............................................................................................................... 35
iv
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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.