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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…
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An outline of the conceptual design features of the proposed 10 MW electron gun-driven
CO2/gas mixture laser is [29]:
• Scalability of total beam output power, beam combining concept.
• Power oscillator or master oscillator-power amplifier (MOPA) design.
• Unstable optical resonator cavity with grating and rotating mirrors beam-combine
techniques.
• Flow and gas handling system with blow down and exhaust to the atmosphere.
• Acoustics suppression with expansion horn downstream and anode muffler.
In this concept there are four separate laser transmitters each generating 2.5 MW
output beams that are combined into a single 10 MW output beam. The oscillator
parameters for each beam transmitter are [29]:
• Energy loading, Ep: Ep = 300 J (higher loadings at reduced gas temperature);
gain volume = 0.27 m 3 (x 4 lasers); A to K = 0.3 m; gain length = 3 m.
• Specific laser output = 65 J/1.
• Estimated extraction efficiency = 20%.
• Pulse repetition rate: 125 Hz@ 20μs.
• Laser power, P = 2.5 MW/beam x 4 beams = 10 MW.
• Laser energy per pulse = 18 kJ/beam x 4 beams = 72 kJ.
• Output wavelengths: 10.6 ~tm, 10.2 ~tm, 9.6 ~tm, and 9.3 μm (mixed).
• Gas mixture ratio (for N2:CO2:H2): 3:1:0.08.
• Gas pressure = 1.013 x 10 5 Pa (or 1 atmosphere).
• Flash factor= 1.3.
The optical resonator cavity and optical components specifications are [29]:
• Resonator type: confocal unstable with rotating mirrors beam combining.
• Magnification, M = 4.
• Cavity length, L = 36.5 m.
• Equivalent Fresnel number = 3.4.
• Cavity end mirrors radius of curvature: RMirror1 = 97.3 m (concave), RM1rror2 = 24.3
m (convex).
• Gain cell: volume= 0.3 x 0.3 x 3.0 m 3 , length= 3 m.
• Beam combine mirrors: 75 x 75 cm 2 flat (30 x 30 cm 2 apertures) @ f. = 10.59
~Lm.
• Low pressure hot cell: 0.3 to 0.5 GHz suppression near line center.
• Output scraper mirror: D = 0.075 m (taped).
See Figure 16 and Figure 17 for schematics of the power oscillator optics and the MOPA.
The laser operation requirements for the gas flow system are (see Figure 18) [29]:
• Flow System: blow down.
• Gain Section
• Cross-section, A= 0.3 m x 3.0 m = 0.9 m 2 .
• Volume, V = 0.3 m x 0.3 m x 3.0 m = 0.27 m 3 .
• Flow speed, u = SO m/sec (@ 125 Hz & flash factor= 1.3).
• Dynamic pressure, !'..P = 2000 Pa (or 0.02 atmospheres).
• Mass flow rate, Q = 60 kg/sec per module ( 45 m 3/sec std).
• Run time, t = 300 seconds
43
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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.