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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. 15 …the Air Force Research Laboratory (AFRL) at Edwards AFB, CA, is for the Ughtcraft to operate…
  • p. 16 …Mead, AFRL/PRSP, Edwards AFB, CA). In the two-mode propulsion concept, a forebody aeroshell acts…
  • p. 18 …Mead, AFRL/PRSP, Edwards AFB, CA). 14 UNCLASSIFIED/ ,'f811. 8ffllilAI! l!llili 8111:¥
  • p. 19 …Mead, AFRL/PRSP, Edwards AFB, CA). UNCLASSIFIED//FQA: QFFIQIO b Wfi&i SU.bl/ 15
  • p. 20 …Mead, AFRL/PRSP, Edwards AFB, CA). Figure 5. Lightcraft Undergoing Horizontal Guide-Wire Flight Test (courtesy…
  • p. 21 …Mead, AFRL/PRSP, Edwards AFB, CA). SUMMARY OF TECHNICAL PERFORMANCE AND BENEFITS We outline below the…
  • p. 73 …In 2005, the AFRL/PRSP (Edwards AFB, CA) concluded their laser Lightcraft propulsion R&DTE program…
  • p. 76 …Force Research Laboratory, Air Force Materiel Command, Edwards AFB, CA. See also, Knecht, S. D., and…
  • p. 77 …Force Research Laboratory, Air Force Materiel Command, Edwards AFB, CA. 35 Salvador, I. I., et al…
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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
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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.