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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 …Ground/Sea-to-Space Concept ............................................................. 27 Figure 15. Air-to-Space Concept ......................................................................... 28 Figure 16. Schematic…
  • p. 31 …Ground/Sea-to-Space Concept: Appropriate rotation of a high-energy laser beam, emanating from a…
  • p. 32 …more than about 10 MW for ground/sea-based lasers, and no more than about 2…
  • p. 33 …SUMMARY AND CONCLUSIONS Ground/Sea to Space (ETO) 261 If laser propulsion can provide nearly all…
  • p. 34 UNCLASSIFIED/ /1"91t 9ffU!l"I!! l!l!il! 8111!!¥ ground, sea and air launches of…
  • p. 37 …favorable for Lightcraft than air-to- ground/sea or air-to-air missions, which are not…
  • p. 39 …to be an attractive alternative to ground/sea-based laser Lightcraft systems. In this case, airborne…
  • p. 43 …would allow detection of most air, land, sea, and space targets, as well as many "low…
  • p. 64 …The Naval Sea Systems Command's (NAVSEA) Directed Energy and Electric Weapon Systems (DE&EWS) Program…
  • p. 67 …Lightcraft nanosat or picosat from the ground, sea, or air, it will be necessary to control…
  • p. 68 …beam train suitable for ground, airborne and sea platforms. • Primary mirror which is also a deformable…
  • p. 71 …to launch laser-propelled Lightcraft from ground/sea to LEO while apertures on aircraft-mounted laser…
  • p. 72 …The entire Lightcraft launch system is comprised of a ground, sea, or airborne laser beam generator…
  • p. 73 …Launching a laser-propelled Lightcraft nanosat/picosat from the ground, sea, or air into LEO requires…
UNCLASSIFIED/ ,'F&II. &FFllilo\l!! l!l!i! 9Hl!!Y
Table 3. Estimated Costs for Hybrid Rocket and Lightcraft Launch Vehicles for
ETO Flight [ 261.
32
3-Stage Hybrid Rocket
Launch Vehicle
Payload ($)
Boosters ($)
Integration ($)
Total($)
Lightcraft Vehicle.f
Ground Based Laser
Lightcraft ($)
Lightcraft Fuel ($)
Laser Power ($)
Laser Refurb. ($)
Total($)
Rocketcraft Cost
Lightcraft Cost
100 Flights
1.0 kg 5.0 kg
Payload Payload
24,948 124,740
399,503 440,927
96,163 101,441
520,615 667,108
1.0 kg 5.0 kg
Payload Payload
24,948 124,740
2,495 12,474
500 2,500
3,000 3,000
30,943 142,714
16.82 4.67
1982 dollars multiplied by 1.62
(2.7% annual inflation) for 2000 dollars
to kg
Payload
250,128
477,131
123,941
851,200
10 kg
Payload
250,128
25,013
5,000
3,000
283,141
3.00
UNCLASSIFIED//FQA: QFFI&l11J.k W&liii Q•lklf

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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.