Documents / Report

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. 3 …Positron Mass .................................................................. 5 Figure 7. LOCAAS Turbojet Engine ......................................................................... 6 iii UNCLASSIFIED//F81it 8FFIIIAI!: 1!181! &••1…
  • p. 4 …Total Positron Requirement for SSRV With a Dry Mass of 60,500 kg ....... 10 Table 4…
  • p. 6 …Hence, when Ps self-annihilates, there is 100 percent conversion of mass into electromagnetic energy given…
  • p. 7 …5 At sea level for a fuel-air mass ratio of 0.068, it is 500…
  • p. 10 …1.00 Positron Mass (mg) ./V 1.50 Figure 6. UAV Range Versus Positron Mass (courtesy…
  • p. 12 …nonstop flights are possible. • Increase in structural mass allows more electronics/passenger amenities. RAMJET-ASSISTED MISSILE…
  • p. 13 …Improving payload mass requires reducing propellant and structural mass, both of which can be accomplished using…
  • p. 14 …GLOW for Chemical SSRV21 Vehicle Component Structure Thermal Protection Propulsion (4 engines) Electronics TOTAL DRY MASS…
  • p. 15 …24 The positron mass budget for a 60,500-kg dry mass for ascension to LEO…
  • p. 17 …First, a reduction in the engine mass for a given thrust is realized; second, there is…
  • p. 19 …lead-cartridge concepts show promise if the mass flow rate of the hydrogen propellant exceeds that…
  • p. 20 …flow-through system with LH2 at higher mass flow rates than LXe; and (d) One-fluid…
  • p. 21 …A separate Brayton-cycle positron energy conversion system provides power to the pellet mass driver and…
  • p. 22 …Comparison of Three Positron Propulsion Concepts for Mars Mission lsp Thrust e+ mass Special Notes Solid…
  • p. 24 …On board propellant requires an overall interplanetary system mass that prohibits use of any type of…
  • p. 25 …This gives significant mass savings or an equivalent reduction in Mars-to-Earth return time for…
  • p. 26 …Mars reference mission 53 , 54 considered payload masses of 60,000 kg for 2015 missions. This…
UNCLASSIFIED/,'P9R: 9PPl!ltllt t!l91!! 9HLY
Figure 10. Artist's Rendition of a Four-Engine Positron SSRV (courtesy of Positronics Research LLC) 26
Positron-Powered Rockets
A positron rocket offers significant advantages over nuclear fission and antiproton
rockets. 27 Nuclear fission reactors contain enormous amounts of highly toxic radioactive
material, and antiproton rockets produce radioactivity in surrounding materials by
interactions of high-energy mesons and gamma rays from antiproton annihilation. The
proposed nuclear fission gas core rocket and anti proton adaptations would release
radioactive fission fragments into the atmosphere. In contrast, positron rockets are
totally radioactivity free.
Second, in the event of an accidental detonation of the positron fuel, the prompt
(nanoseconds) burst of gamma rays can be shielded from humans on spacecraft. The
1/e absorption length of a 511-keV gamma ray in lead is 5.6 millimeters. A 13-
centimeter (cm)-thick shield thus reduces the gamma ray flux by a factor 8.3 x 10-11 .
To illustrate, a human behind such a shield at a distance of 10 meters from a 100-mg
source of annihilating positrons would experience a whole-body radiation dose of 2 rem
(roentgen equivalent man), which is within the annual tolerance for radiation workers in
the United States.
The following sections investigate three positron rockets: solid core, gas core, and
photon. 28 In a solid-core positron rocket, positrons heat a hydrogen working fluid
through an attenuating solid such as tungsten. In a gas-core positron rocket, gamma
rays directly heat propellant through a one- or two-fluid process. In a photon positron
rocket, solid propellant is ablated from a surface bombarded by gamma rays.
11
UNCLASSIFIED,' /P8"1 8PPll!l"'I! l!l!il! 8111!¥

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. 35 pages are in the text index: search them above, or from the library's search.