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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. 8 …The sensor must be capable of detecting Earth over a range of orbital radii with a…
  • p. 17 …For the purpose of this report, we envision a Lightcraft Earth-to-Orbit (ETD) transportation system…
  • p. 34 …not only placing nanosats into LEO at low cost (Figure 14), but also for performing much…
  • p. 42 …Each picosat is gravity- gradient stable, has a dipole array facing Earth, and a broader beam…
  • p. 43 …811L¥ push broom scanning mode for complete Earth coverage rather than only sampling coverage. The constellation…
  • p. 72 …The system is single-stage-to-orbit and completely reusable with no onboard propellant required (the…
  • p. 75 …J., et al. (1991), "System Requirements for Low-Earth-Orbit Launch Using Laser Propulsion," in Proc…
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• Average power limited by low thermal conductivity of host material.
• Wavelengths propagate extremely well in clear weather:
- Very low absorption.
- Higher scattering.
The requirements for high average power bulk solid-state lasers are [30]:
• Efficient optical pumping of gain medium:
- Flash lamp or laser diode well matched to absorption band.
- Small wavelength difference between pump and lasing ➔ low quantum defect.
• Efficient heat removal from gain medium:
- Improved heat removal techniques from host.
- Large surface area per unit volume.
- Or, large volume to store heat with low duty cycle operation.
• Gain medium must retain good (correctable) optical quality.
The typical properties of widely used Nd :YAG lasers are [30]:
• 4 nm absorption line width.
• 24% heating from quantum loss.
• Saturation intensity:::: 3 kW/cm 2 (at:::: 2% dopant).
• Multi-kilowatt average power demonstrated.
• Maximum average power potential ~ several hundred kilowatts:
- Heat removal makes continuous running a challenge at this power.
- Current high-energy SSLs produce great amounts of heat (e.g., 600 kW of
electrical power in and 100 kW of beam power out equals 500 kW of waste
heat).
- Must store the waste heat and reject it from the system at a lower rate, thus
requiring storage and limited duty cycle.
• Quantum defect= pump light photon energy minus laser light photon energy.
The typical properties of widely used Yb:YAG lasers are [30]:
• 18 nm absorption line width.
• Indium gallium arsenide (InGaAs) pump laser diodes at 0.941 μm wavelength:
- 8.6% heating from quantum loss.
• Saturation intensity:::: 9.7 kW/cm 2 (at:::: 25% dopant).
• Multi-kilowatt average power demonstrated.
• Maximum average power potential is perhaps 5 x Nd:YAG laser.
A new technology that enables the scaling-up of BSSSL beam power is a recently
developed thermal management system that is used to remove and store the waste
heat produced by BSSSL devices. General Atomics' Advanced Power Systems Division
recently announced* that it has completed testing of an advanced thermal energy
·Reported in Space War Newsletter, June 7, 2010.
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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.