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Defense Intelligence Reference Document Space Access Where We ve Been And Where We Could Go

Defense Intelligence Agency · 56 pages · text from the file's own layer

This Defense Intelligence Reference Document, prepared by the Defense Intelligence Agency and dated 8 March 2010, was produced under the Advanced Aerospace Weapon System Applications (AAWSA) Program. It gives a historical and technical review of how to reach space and return. It covers hypersonic gliders, air-breathing and rocket propulsion, thermodynamics and materials, and launch options. It argues that reliable, schedulable access to low Earth orbit is mainly a hardware and propulsion problem rather than a technology one.

  • p. 2 …FY 2009 Advanced Aerospace uestions pertaining to AAWSA Program Bldg 6000, Washington, under the Defense Intelligence…
  • p. 5 …Among the many advances in space access that will be possible in the future,' the key…
  • p. 10 UNCLASSIFIED/,Sf81il 8ffll!ltllt ~!II!! SHLY McDonnell Aircraft Advanced Design Dept. 1958 to 1967 Mr. H…
  • p. 11 …Louis) Advanced Design organization. The vehicle concept initially conceived in the late 1950s and early 1960s…
  • p. 23 …The photo in Figure 16 is from a Society of Automotive Engineers book titled Advanced Engine…
  • p. 30 …to advance beyond a demonstration tube ended in frustration. Any attempt to open the tube results…
  • p. 32 …Propulsion The photo in Figure 27 is from the Society of Automotive Engineers book, Advanced Engine…
  • p. 38 …These solution areas represent the entire propulsion spectrum, from all-rocket (far right) to advanced air…
  • p. 39 …the launcher can return with payload and fuel residuals onboard), use legacy correlations from McDonnell Advanced…
  • p. 45 …why have we advanced so little (as illustrated in Figure 43)? Like the pioneers' Conestoga wagons…
  • p. 47 …to advance beyond a solitary orbital station with limited capabilities. Figure 44 identifies the elements necessary…
  • p. 56 …6 KOchemann, D., "The Aerodynamic Design of Aircraft - A Detailed Introduction to the Current Aerodynamic Knowledge…
UNCLASSIFIED/ /PS"-. 9PPl!ltllt t!l91!! 9HLY
The Qu Tube
In the 1990s, a colleague, Ying-Ming Lee, who then worked at MSE in Butte, Montana,
showed the author a copper tube about a foot long that was a heat pipe from his
colleague in Taiwan. If the tip was put into a cup of hot water, the other end almost
instantly was too hot to hold. If it was quickly put into a glass of cold water, that tip
just as quickly became ice cold. As documented in the excerpted page below from the
University of Alabama, Huntsville, Annual Report, the apparent conductivity is greater
than copper and could not be melted, as the thermal energy would be removed so fast
that a significant temperature rise could not be attained. This could have significant
industrial application for the United States. The late Clark Hawk had obtained a 10-
foot-long Qu tube and tested it in his laboratory. The results were published in the
University of Alabama, Huntsville, Annual Report. However, as Clark Hawk discovered,
the Chinese team associated with Professor Qu in mainland China was not about to let
this discovery into American hands. Plus his team was composed of a number of
young, ambitious technocrats who thought they knew how to make their fortune. So
both Ying-Ming's and Clark's attempts to advance beyond a demonstration tube ended
in frustration. Any attempt to open the tube results in failure, as whatever is in the
tube reacts into an inert powder. The author has two smaller tubes in his possession.
With applications including hypersonic vehicles, nuclear power plants, and electronic
cooling, these devices would lead to an economic breakthrough in practical thermal
control.
23
UNCLASSIFIED/ ;CEiOAt OFFIQI.Ctk Wlii &••LY

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Report, from the dia collection. The PDF is mirrored here; the original link is above. 56 pages are in the text index: search them above, or from the library's search.