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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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A novel new HEL beam control architecture being tested and deployed by the various
directed energy weapons programs that offers reduced complexity and component
count, and combines many functions into a compact arrangement has the following key
features:t=
• End-to-end boresight tracker with 0.1 micro-radian root-mean-square accuracy at
10 KHz.
• No beacon illuminator laser (BILL) required.
• Real-time beam quality measurements on target during each engagement.
• Extremely compact and lightweight beam train suitable for ground, airborne and
sea platforms.
• Primary mirror which is also a deformable mirror (DM) and a fast steering mirror
(FSM).
•Chemical
• Solid-State
• Free-Electron
L~ser Device
Module
IIIIIIR:,-
Alignment
Sensor
'"Inertial
Platform
,.,,~.r[ '-J~Mirror Waverront Traclt.-roc~I
I Sensor Plane
I
Defom,able -~,1-._ _ _ (',
M1rrer 1" ,,.,I I
•
Local-loop
. I,.,_ Wavefront
,, Sensor
Propagation
Through
Atmosphere
(or space)
Figure 33. Notional Long Range HEL Beam Control System (courtesy of the Directed Energy
Professional Society).
64
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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.