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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…
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are described by the Rankine-Hugoniot
thermodynamic properties.
equations, which yield the ratio of certain
Expansion Fan Bow Shockwave
B
I Region 2 I Region 1 I
M,> 1
Figure 4. Supersonic Flow Past a Wedge-Shaped Body.
Turbulent Wake Detached Shock
Expansion Fans
Blunt Body
Figure 5. Supersonic Flow Past a Blunt Body (Spheroid).
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