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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. 2 …a series of advanced technology reports produced in FY 2010 under the Defense Intelligence Agency,~(b…
  • p. 5 …the mission operational costs for tracking and managing a constellation. To reduce overall mission cost, advanced…
  • p. 8 …being the biggest drivers. Advanced microelectronic solutions are being developed to meet these challenges. The microelectronics…
  • p. 9 …The RHrFPGA also allows concurrent design by decoupling the logic design from the module, shortens the…
  • p. 12 …However, "receiver-on-a-chip" technology has advanced to the point where including a receiver onboard…
  • p. 17 …the NASA-Marshall Space Flight Center and the Propulsion Sciences and Advanced Concepts Division of the…
  • p. 55 …remove and store the waste heat produced by BSSSL devices. General Atomics' Advanced Power Systems Division…
  • p. 56 …The HELLADS matched-index- of-refraction liquid cooling technique and General Atomics' advanced thermal energy storage…
  • p. 64 …and testing of advanced high-energy/high-power FEL designs for the purpose of deploying them…
  • p. 66 …High-Power FEL Optical Resonator (courtesy of the Naval Post-Graduate School FEL Lab). ESTIMATED PAYLOAD…
  • p. 72 …The system is single-stage-to-orbit and completely reusable with no onboard propellant required (the…
  • p. 75 …Laser Propulsion Q Advanced Applications," in Vision-21: Space Travel for the Next Millennium, edited by…
  • p. 76 …Advanced Concepts Office, AFRL/PRSP, Edwards AFB, CA (Nov. 18, 2002). 30 Kalisky, Y. (2006), The…
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1,000 nanosats attached to the tether. Each nanosat is a self-contained optical sensor
spacecraft, integrated into a 0.1 kg package. The sensor thus detects 1,000
wavelengths simultaneously. The sensor has a resolution as small as 40 cm on the
ground from GEO. Its field of view can be scanned over an area by tilting the ensemble
using MEMS FEEP thrusters on the nanosats, or libration modes can be excited in the
tether so that the field of view scans across a 2,000 km coverage area in a quasi-
random mode, eventually covering the entire area. These thrusters also serve for
stationkeeping. Its total weight is less than 900 kg in orbit, which can be reduced in
the future to 9 kg if Buckytubes are used to construct the system.
41
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Report, from the dia collection. The PDF is mirrored here; the original link is above. 77 pages are in the text index: search them above, or from the library's search.