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Defense Intelligence Reference Document Detection And High Resolution Tracking Of Vehicles At Hypersonic

Defense Intelligence Agency · 46 pages · text from the file's own layer

This Defense Intelligence Reference Document from the Defense Intelligence Agency, dated 20 November 2010, was one of a series of advanced technology reports produced in FY 2010 under the Advanced Aerospace Weapon System Applications (AAWSA) Program. It reviews the theory of subsonic, supersonic and hypersonic flow. It then compares electromagnetic, optical, and acoustic and seismic methods for detecting and tracking hypersonic objects, and it makes four recommendations for progress over the next 30 years.

  • p. 11 …V=J8:T (9) For air near sea level (p = 101,320 Pa, T = 293 K…
  • p. 13 …traveling at Mach 3 through air at sea level, the pressure in the region between the…
  • p. 17 …II for the detection of aircraft and sea vessels. First patented by Christian Hulsmeyer in 1904…
  • p. 23 …C), the pressure is 26.1 % of sea level atmospheric pressure (see Appendix A for the…
22
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Peak Wavelength of Emitted Radiation
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Figure 15. Peak Wavelength of the Infrared Radiation Emitted by Hypersonic Objects.
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Temperature Downstream of a Normal Shock
Above 550C (823 K), Ionization and
D1sassociat1on of Oxygen and
Nitrogen Lead to Lower
Temperatures in the Gases
Downstream of the Bow Shock .
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Figure 16. Peak Shock Layer Temperature for Hypersonic Objects.
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Report, from the dia collection. The PDF is mirrored here; the original link is under it. 46 pages are in the text index: search them above, or from the library's search.