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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…
UNCLASSIFIED//F&II. &FFiii,111!! l!llili &HI!¥
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
UNCLASSIFIED/ /Pett err1e1111t ~:!I! 9HLY

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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.