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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. 4 …Influence of Target Velocity and Intercept Angle on Impact Energy and Required Mass .................................................................................................. 33 Table 5…
  • p. 5 …The term "minisatellite" refers to a spacecraft with a wet mass (including onboard propellant) of 100…
  • p. 7 …Nanosatellite Technologies OVERVIEW Nanosats require technologies that radically reduce the mass and power of components without…
  • p. 8 …nanosat presents some unique challenges, with low mass (0.25 kg) and low power (0.5…
  • p. 9 …In order to develop a low mass C&DH, a lightweight and low power electronics packaging…
  • p. 11 …RF COMMUNICATIONS The onboard RF subsystem must be small, low mass, and low power. The system…
  • p. 12 …additional strain on an already challenged nanosat mass and power budget. For this reason, the concept…
  • p. 13 …The material will be selected based on mass, cost, manufacturability, ease of assembly and integration, and…
  • p. 15 …for the spacecraft because a large propellant mass and heavy energy source are not carried onboard…
  • p. 17 …Current Lightcraft designs are limited to about 60 g mass and 15 cm in diameter by…
  • p. 21 …It requires a beam power of 0.1 to 1 MW per kg of vehicle mass…
  • p. 22 …The majority of the system mass required to launch a payload to orbit is left on…
  • p. 24 …Therefore, this would allow approximately 4 kg of mass to be placed into orbit with the…
  • p. 25 …same ply-thickness) to meet Lightcraft airframe mass requirements. Another important finding in the study was…
  • p. 31 …Additional estimated mass for performing the Lightsat function is no more than about 1 kg, if…
  • p. 32 …Lightcraft takeoff masses no more than about 20 kg can be accelerated to orbital velocities by…
  • p. 33 …for missile and maneuvering aircraft interception. • Additional mass along Lightcraft centerline for hardened target penetration. LIGHTCRAFT…
  • p. 34 …Lightcraft sizing assumed a propellant mass fraction of 0.5 and 1.0 MW of laser…
  • p. 35 …Hybrid Rocket Expendible Launch Vehicle - Assumed Perfonnance and Estimated Weights Payload Mass (kg) 1.00 5…
  • p. 37 …It is therefore estimated that the air-to-space Lightcraft dry mass would be about the…
  • p. 38 …Influence of Target Velocity and Intercept Angle on Impact Energy and Required Mass 2 61. Lightcraft…
  • p. 39 …Influence of Lightcraft and Target Velocity on Impact Energy and Required Mass 261. Lightcraft Lightcraft Impact…
  • p. 40 …The lower mass also saves launch costs, so the total system costs less for the same…
  • p. 41 …many spacecraft that the economics of true mass production will come into play in space for…
  • p. 44 …the local vertical, with its center of mass in GEO. The Fresnel zone plate has a…
  • p. 46 …wall plug and optical efficiencies, cost, complexity, mass, and size. Free-electron lasers are another class…
  • p. 47 …P = 2000 Pa (or 0.02 atmospheres). • Mass flow rate, Q = 60 kg/sec per module…
  • p. 48 UNCLASSIFIED//509 AEEJCJOP 11£5 O.-blf + Total mass flow rate, Qtota1 = 240 kg/sec for…
  • p. 50 …sec, and 15 kg/sec of CD2 mass flow represents 2.053 x 1026 molecules/sec…
  • p. 51 …The 60 kg/sec mass flow requirement of the 3: 1 N2/C02 lasing gases means…
  • p. 53 …mass (not including the prime power and cooling systems) to achieve the low specific mass (5…
  • p. 65 …is the undulator period, mis the electron mass, and c is the speed of light. 'MeV…
  • p. 72 …The Lightcraft specific impulse is essentially infinite (several thousand seconds in rocket mode), while payload mass…
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achieved by laser weapons with 25 kW or 50 kW beam power, provided the energy is
transmitted with good beam quality. Laser propulsion requires megawatt-class lasers
which are only developed in directed energy weapons (DEW) programs. However,
BSSSL beam power can be scaled up further by improving presently known gain media
and doping combinations, inventing new gain media and doping combinations, by
combining the beams of several lower-power devices, or a combination of all these until
the ultimate optical/thermal/mechanical limit of slab gain materials is reached. BSSSL
beam output power is projected to reach the multi-megawatt level within three to five
years from the time of this writing (P. Zarubin, J. Albertine, and V. Hasson, private
communications, 2010).
Figure 20 shows DARPA's High Energy Liquid Laser Area Defense System (HELLADS) as
an example of a liquid-cooled bulk slab solid-state (ceramic) laser. HELLADS is
designed to be light and compact enough to fit on a jet fighter or drone aircraft, and yet
powerful enough to fire a 150 kW beam of energy. HELLADS makes use of a unique
cooling technique to save weight and size. The high-power laser uses a liquid that has
the same index of refraction as the mirrors inside the laser. That way, the laser can
fire away, even while it's being cooled. The HELLADS program will deliver a 150 kW
laser weapon at 2 m 3 of system volume and 600 kg of system mass (not including the
prime power and cooling systems) to achieve the low specific mass (5 kg/kW) and
compact size need to be mounted on small tactical airborne platforms like the C-130
transport, jet fighters, or Predator-class UAVs. The device will be built by General
Atomics and the tracking system will be built by Lockheed-Martin.
A bulk solid-state laser is based on a bulk piece of doped crystal, disordered or
amorphous material (such as glass), glass ceramic (which is a combination of
crystalline-ordered structure and glassy phases disordered structure), or mixed crystals
as the laser gain medium. In most cases, the gain medium is doped either with rare-
earth ions or transition metal ions. Typically, these ions replace a small percentage of
other ions of similar size in the host medium. The laser-active ions have suitable
optical transitions for pumping and laser emission at wavelengths where the host
medium is transparent. A bulk laser resonator is often formed with laser mirrors placed
around the gain medium. However, there are also laser gain media with a highly
reflective dielectric mirror coating on one side, which serves as a resonator end mirror.
Also, there are monolithic solid-state lasers where the beam path is entirely inside the
gain medium. See Reference 30 for additional technical details.
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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.