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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 …Free-Electron Laser Electron Beam Phase-Space Evolution ....................... 59 Figure 31. Recirculating-Beam FEL System ........................................................... 60…
  • p. 4 …HEL Beam Pointer/Tracker ................................................................... 65 Figure 35. Basic Shared Aperture Beam Control System ......................................... 66 Figure 36…
  • p. 7 …This can only be achieved via laser propulsion in which the laser beam energy that is…
  • p. 15 …By launching spacecraft on a beam of electromagnetic radiation, researchers will have developed the first new…
  • p. 16 …The laser beam's pulse interacts with the mirror, spreading out and focusing into an annular…
  • p. 17 …1) power supply; 2) high-power (megawatt-class) laser beam generator/transmitter using novel beam optics…
  • p. 20 …is to the right and the laser beam strikes the stretched-out parabolic mirror/propulsion section…
  • p. 21 …It requires a beam power of 0.1 to 1 MW per kg of vehicle mass…
  • p. 22 …The ground-based megawatt-class laser beam generator is state-of-the-art technology. The cost…
  • p. 25 …Figure 8 illustrates the adverse beam propagation geometry associated with ETO laser propulsion by means of…
  • p. 26 …Attenuation Effects on Captured Laser Beam Power 261. 0.4 0.J 0.2 0.1…
  • p. 27 …Unfortunately the demonstrated laser beam power levels for the attractive 1.62 μm wavelength, which suffered…
  • p. 28 …Beam combining of several 1 MW (or higher) FELs can achieve a total combined beam output…
  • p. 31 …Appropriate rotation of a high-energy laser beam, emanating from a ground/sea-based laser, guides…
  • p. 32 …Appropriate rotation and translation of a high-energy laser beam, emanating from a moving aircraft, guides…
  • p. 33 …But multiple target interception within allowable time is limited by relatively long beam- riding time needed…
  • p. 37 …In this case, it is envisioned that the high- pulsed power within high-energy laser beams…
  • p. 39 …In this case, airborne laser beams at 12 km altitude will not suffer the significant propagation…
  • p. 41 …sidelobes, creates multiple beams, and steers the ensemble of the individual beams anywhere on Earth. The…
  • p. 42 …Each picosat is gravity- gradient stable, has a dipole array facing Earth, and a broader beam…
  • p. 43 …Commands for beam sweep delays are superimposed on the time delays of each nanosat. Each nanosat…
  • p. 44 …piezoelectric membrane kept flat by an electron beam in response to an optical figure sensor. MEMS…
  • p. 46 …technical issues include large wavelength and atmospheric absorption of the laser beam. • Carbon Monoxide (CO) Laser…
  • p. 47 …125 Hz@ 20μs. • Laser power, P = 2.5 MW/beam x 4 beams = 10 MW. • Laser…
  • p. 50 …Each power oscillator optics module transmitting a 2.5 MW beam of 10.6 μm wavelength…
  • p. 52 …Adding an eight amplifier chain that the system was designed for will increase the beam power…
  • p. 53 …However, BSSSL beam power can be scaled up further by improving presently known gain media and…
  • p. 54 …scalable to 1 MW beam power within 2 years. Typical solid-state lasers have the following…
  • p. 55 …A new technology that enables the scaling-up of BSSSL beam power is a recently developed…
  • p. 56 …at the same time increasing the average beam power. Figure 21. Phase Change Materials Allow Storage…
  • p. 57 …This exponential growth in beam output power is the result of many factors, including the parallel…
  • p. 58 …Microlens -O _ ,:1 Incoherent Beam Combining 'Ind1vidually Incoherent Gaussian Beams i=L Controlled /_/Steering • ... o~bined…
  • p. 59 …Neodymium Thulium (Tm 3+), Holmium - Range of beam wavelengths(),) produced: 0.48 μm to 2.9…
  • p. 61 …Multlmode Fiber Lasers 50kW Multimode Output beam quality BPP-1 o M"2-33 DC EDE…
  • p. 62 …The resulting laser beam photon energy depends on the electron energy, the undulator period, and (weakly…
  • p. 63 UNCLASSIFIED/ /F8~ 8FFl&I.«1k WliEii a,.klf electron beam ( \ I,:--- ■■>ti■-- undulator ) resonator mirror 0…
  • p. 64 …The superconducting accelerator gives good efficiency and gradient while recirculation of the electron beam recovers beam…
  • p. 65 UNCLASSIFIED/ /F&~ 8FFHiil.«1k 1!181! &••kY - K"' 1.5.t • Electron Beam: - Photocathode injector creates…
  • p. 66 …HIGH ENERGY LASER BEAM CONTROL ··costs could be reduced to as low as $20 per kg…
  • p. 67 …The typical HEL beam control system includes:++ 1) a gimbaled beam director, 2) tracking and pointing…
  • p. 68 UNCLASSIFIED//F&II. &FFiii,111!! l!llili &HI!¥ A novel new HEL beam control architecture being…
  • p. 69 …HEL Beam Pointer/Tracker (courtesy of the Directed Energy Professional Society). In summary, this new architecture…
  • p. 70 …The BILL is a solid-state, kilowatt-class laser that measures atmospheric conditions, allowing the beam…
  • p. 71 …All of these HEL beam control innovations can be quickly adapted to laser propulsion applications with…
  • p. 72 …The entire Lightcraft launch system is comprised of a ground, sea, or airborne laser beam generator…
  • p. 73 …New beam control devices and high-power optical train combinations have a resulting beam line that…
  • p. 75 …N. (1983), "Advanced Beamed-Energy and Field Propulsion Concepts," BDM/W-83-225-TR, BDM Corp…
  • p. 76 …N. (2001), "World Record Flights of Beam-Riding Rocket Lightcraft: Demonstration of 'Disruptive' Propulsion Technology," AIAA…
  • p. 77 …of the 6 th Int'! Symposium on Beamed Energy Propulsion, edited by C. R. Phipps, AIP…
UNCLASSIFIED//F&A 8FFl&I.«1k WliEii a,.klf
In order to launch a laser-propelled Lightcraft nanosat or picosat from the ground, sea,
or air, it will be necessary to control and steer the high-energy laser (HEL) beam, while
at the same time making real-time adjustments to account for platform motion, optical
train and atmospheric effects on beam propagation, so that the beam maintains high
quality, low-loss, precision contact with the Lightcraft from launch all the way up to
LEO. While the atmospheric effects on laser beam propagation were briefly discussed
in the Lightcraft Nanosatellite Configuration section of Chapter 2, a more in-depth
examination of this phenomenon can be found in Reference 32. In what follows, we
briefly discuss what a HEL beam control system is designed to do and what innovations
were recently developed by the various DoD directed energy weapons programs that
are just now being successfully tested and deployed.
A beam control system is designed to:tt
• Acquire and precisely track a designated target.
• Handles the HEL beam emitted from the laser:
- Aligns the HEL beam to the optical train's axis - from the laser resonator to the
beam director's exit aperture.
- Safely relays the HEL beam through the optical train with minimal loss of
energy and beam quality.
• Expands the HEL beam and focuses it at the range of the target.
• Places and maintains the HEL beam on the desired target's aimpoint.
• Corrects for beam quality degradations in the optical train or the atmosphere (if
needed).
HEL weapons usually have high-power optical trains containing more than a dozen
mirrors. However, these systems need to be far more compact with minimal high-
power trains. As directed energy weapon applications begin to employ smaller HEL
systems, the size, weight and complexity of the accompanying beam control system
has come down as well. The typical HEL beam control system includes:++ 1) a gimbaled
beam director, 2) tracking and pointing functions, 3) adaptive optics, 4) acquisition
sensors, and 5) target illuminators. Solutions have been recently developed to drive
towards a smaller, lighter and simpler beam control system while considering the entire
end-to-end system architecture. Existing beam control solutions are robust but large
and complex. The technical strides achieved in the past 20 years in wavefront sensing,
aperture sharing elements, beam tracking and beam correcting provide new tools to
offer a simplified low mirror count beam control system while retaining the ruggedness
of function necessary for a laser weapon.
Figure 33 and Figure 34 show schematics of a notional inertially-stabilized
pointer/tracker mount and beam control system that was developed by NAVSEA's
DE&EWS Program.
,-o. Kiel, Directed Energy Systems Symposium Short Course, Naval Post-Graduate School, Monterey, CA, 2010.
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D. Kiel, Directed Energy Systems Symposium Short Course, Naval Post-Graduate School, Monterey, CA, 2010.
UNCLASSIFIED//F8A 8FFI&II k WEEii ,u1uc 63

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