Documents / Report

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/ ,'f811. 8ffiliii,r.k I.Iii O•lk¥
>. ""(
_..I
Figure 6. Lightcraft Undergoing Horizontal Guide-Wire Flight Test (courtesy of F. Mead,
AFRL/PRSP, Edwards AFB, CA).
SUMMARY OF TECHNICAL PERFORMANCE AND BENEFITS
We outline below the propulsion performance features of the laser Lightcraft launch
system:
• The system is single-stage-to-orbit and completely reusable.
• Almost no onboard propellant is required (the reaction mass is free air), except
for the small internal amount of propellant needed for final ascent to orbit and
orbital maneuvering.
• Vehicle specific impulse (Isp) is essentially infinite ("' several x 10 3 seconds in
rocket mode).
• Payload mass fractions are"' 50 - 95%.
• These systems are simple, reliable, safe, environmentally clean, and could have
a very high all azimuth on-demand launch rate.
• Reduces space launch costs by two to three orders of magnitude below today's
levels: estimated launch costs are $20/kg to $600/kg of payload (not including
life cycle and launch operations costs).
• The feasibility and physics principles have been proven by the AFRL's Lightcraft
Concept Demonstration Program [11, 16-25].
Lightcraft systems have sufficient power density to operate as ETD launch systems. It
requires a beam power of 0.1 to 1 MW per kg of vehicle mass, while orbit-to-orbit
17
UNCLASSIFIED//F81il 8FFI&I.t.k Wlili a,.k\f

Not linked to a story yet.

About this file

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.