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Defense Intelligence Reference Document Positron Aerospace Propulsion

Defense Intelligence Agency · 35 pages · text from the file's own layer

This unclassified Defense Intelligence Reference Document from the Defense Intelligence Agency is dated 2 March 2010. It was produced in FY 2009 under the Advanced Aerospace Weapon System Applications (AAWSA) Program. The report reviews work on using positrons as aerospace fuel. It covers air-breathing turbojet and ramjet engines, unmanned aircraft, missiles, single-stage reusable vehicles, positron rockets and a crewed Mars mission, along with how positrons could be produced and stored. It concludes that a first positron-powered flight around the globe could be possible within 10 years.

  • p. 5 …This paper is an anthology of that work and not a general review of antimatter propulsion…
  • p. 7 …Because of the aforementioned performance bounds of combustion engines, the aeronautic industry has worked diligently to…
  • p. 13 …Defense, NASA, and the aerospace industry are working to eliminate multistage rockets for access to low…
  • p. 16 …28 In a solid-core positron rocket, positrons heat a hydrogen working fluid through an attenuating…
  • p. 18 …heated H: • Propellant-heated He • Working fluids for power • Working fluids for power systems - inert gas…
  • p. 21 …was assumed to be parabolic for this work. 38 To make the Sanger photon rocket practical…
  • p. 22 …be possible • Hot-bleed line possible Future work • Efficiency study Gas-Core Sanger Ablation 1000 - 2500…
  • p. 23 …consumption does not dominate rocket positron consumption. ◄ Work 5 Rf'!gf'l'M'rllto.- JC~ ~ 4…
  • p. 31 …What lifetimes might be expected working Figure 22. TEM of Silica Aerogel (courtesy with this material…
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POSITRON ENERGY CONVERSION FOR ONBOARD POWER
Research was conducted on positron utilization in a standalone, closed-loop, high-power
system. 42 A Brayton cycle engine (Figure 14) was investigated with output power of 100
kW, consistent with Mars Reference Mission specifications. 43 , 44 Results show efficiencies
of 25-30 percent and positron consumption of 7 μg/hour.
Such a power system would have practical meaning for fast transits to Mars where
positron consumption does not dominate rocket positron consumption.
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Figure 14. Closed Brayton Cycle Using Positron Annihilation (courtesy Positronics Research LLC) 45
In addition, a small, 110-watt, positron-driven generator (Figure 15) for small, onboard
tasks was designed around the NASA Glenn Research Center Stirling Radioisotope
Generator,46 with heat provided by Ps gamma rays.
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: k ,, ,: •I,~ ,i ,-, •
St,r11ng Convertor 1(55 We) Slirlrng Convcrto, 2 {55 We)
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Figure 15. Conceptual 110-Watt Positron Closed-Cycle Generator Based on the NASA Glenn Research
Center Stirling Radioisotope Generator47 (courtesy Positronics Research LLC) 48
18
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Report, from the dia collection. The PDF is mirrored here; the original link is under it. 35 pages are in the text index: search them above, or from the library's search.