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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. 5 …the per-unit cost will be reduced to a small fraction of UNCLASSIFIED//F8A 8FFIQIOP !PSS…
  • p. 8 …Advanced microelectronic solutions are being developed to meet these challenges. The microelectronics developed must be modular…
  • p. 9 …The packaging method that will be chosen must have a small volume and small footprint (6…
  • p. 11 …This reduction will be accomplished by leveraging recent successful tests of a small cryogenic two-phase…
  • p. 13 …methods should be developed to verify quality and structural performance by testing a small subset of…
  • p. 22 …The dry spacecraft mass can be further reduced by two orders of magnitude, and thus the…
  • p. 24 …further indicated that small COTS chemical propulsion systems, with sufficient thrust, would be about a factor…
  • p. 32 …Lightcraft takeoff masses no more than about 20 kg can be accelerated to orbital velocities by…
  • p. 37 …Eliminating such satellite threats has not been examined in detail, but they could be rapidly eliminated…
  • p. 40 …A generic description would be a constellation of small spacecraft each performing its separate function, but…
  • p. 41 UNCLASSIFIED/,, OK 01 I ICIAE 652 one I These array functions can be made coherent over…
  • p. 42 …The coverage spot diameter can be varied by choosing the diameter of the array that is…
  • p. 43 …The relative positions of these picosat elements changes slowly, and only small and infrequent stationkeeping propulsive…
  • p. 44 …can be emplaced and replaced incrementally using laser- powered Lightcraft launch vehicles or even small conventional…
  • p. 45 …small as 40 cm on the ground from GEO. Its field of view can be scanned…
  • p. 50 …use N2, CO2, and small quantities of H2. • Subscale testing will be used to anchor the…
  • p. 53 …kW) and compact size need to be mounted on small tactical airborne platforms like the C…
  • p. 72 …This would be a constellation of small spacecraft each performing its separate function, but these functions…
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that has runways of reasonable length. An air-launched Lightcraft launch vehicle
mission, involving the transport of lasers and Lightcraft on medium-sized bombers or
transport aircraft, is also recommended if additional funding would become available.
FUTURE NANO-/PICO-SATELLITE MISSION CONCEPTS
Coherently cooperating "swarms" are a novel innovation for replacing structures with
information by placing many formation-flown small satellites into a loose "swarm" and
cause them to cooperate coherently. This is very different from the so-called
distributed small satellite LEO constellations currently pursued in which individual small
spacecraft perform essentially the same functions as larger satellites but at lower
spacecraft mass ( or weight) and cost. These smaller spacecraft can be proliferated to
provide greater geographical coverage for the same cost. The lower mass also saves
launch costs, so the total system costs less for the same function performed with larger
spacecraft.
In contrast, the swarms, as described in the following sections, cooperate coherently
and form a real distributed system in which the whole is more than the sum of the
parts. A generic description would be a constellation of small spacecraft each
performing its separate function, but these functions combine to create at a central
location a much larger virtual spacecraft, or sensor aperture, that exists solely because
of the cooperation of the spacecraft. The following sections provide several examples
of the implementation of such systems in which each of a large number of small
satellites in a swarm or other constellation will radiate or receive signals and combine
them in phase, or coherently, regardless of their actual location in orbit. This creates
coherent RF or optical apertures that are essentially unlimited in size.
Each satellite's position is only crudely station kept, and the satellites adjust the time
delay or phase delay of the signals they repeat to compensate for their position errors,
causing their repeated signals to add coherently at a collection point. This technique
can be easily applied to RF transmitters and receivers, and with more demanding
accuracy to optical transmitters and receivers. The result in either case is a large
"swarm" or loose constellation of satellites that act as one large antenna or optical
array, even though they are separate and their positions are neither constant nor lie
along a parabola or plane in space. The individual satellites can be as simple as one-
element flying chips or as complex as today's self-contained sensing spacecraft of
various sizes.
The advantage of coherently cooperating distributed systems is that they can form
sparse RF antennas and optical sensors with diameters so large that they would be
impossible to implement with filled apertures even if formed with adaptive membranes;
and have orders of magnitude smaller mass. The relative locations of individual
spacecraft in the swarm can be controlled by MEMS FEEP propulsion, tethers, or by
cleverly conceived orbits in which the elements of the array appear to orbit a common
center within it, thus eliminating the need to use propulsion at least for first order
station keeping.
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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.