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The Roswell Report: Fact vs. Fiction in the New Mexico Desert

USAF / The Black Vault · 1995 · 882 pages · text by OCR

The Roswell Report: Fact versus Fiction in the New Mexico Desert was published by Headquarters United States Air Force in 1995. The Black Vault distributes this copy. It reproduces the report by Col. Richard L. Weaver and the synopsis by 1st Lt. James McAndrew, both written after a General Accounting Office inquiry requested by Representative Steven Schiff. The Air Force search found no evidence of an extraterrestrial craft or crew. It concluded that the Roswell debris most likely came from NYU Flight No. 4, a Project MOGUL balloon train.

  • p. 39 …An advance ground team, led by Albert P. Cray, preceded the NYU group to Alamogordo Army…
  • p. 96 …OSI also developed an advanced Narcotics Investigations Course designed to teach the latest technics in combatting…
  • p. 174 …Dr Crary and Dr Peoples were the advance people and scientific monitors for our project. Dr…
  • p. 247 …Spilly was a consultant, and even in his advancing age he was still an enormous source…
  • p. 273 …the advance party of the balloon group arrived by B-17. $ ^{21} $ On May 29, the…
  • p. 617 …in advance of balloon release and a second notice will be filed at the time of…
  • p. 618 …Upon attaining the desired altitude, the auxiliary lifting balloons will be released from the main balloon…
  • p. 694 …in advance of balloon release and a second notice will be filed at the time of…
  • p. 695 (1) The type balloon to be used in this phase of the project will be a…
A glass flask is open to atmospheric pressure through a fine capillary tube. With various rates of change of pressure, various differential pressures exist between the air in the flask and the outside air. This pressure difference controls the level of liquid in a manometer switch, filled with 24% hydrochloric acid. When the internal pressure is 0.2 mb more than the ambient pressure, the switch opens and ballast flow is stopped even though the balloon may be below the floating level. (The switch is set so that a rate of change of .1 mb/minute acting for three or more minutes will open the switch.) By thus restricting flow when the balloon is rising, balloon oscillations are minimized and ballast is conserved. A sketch of this operation is shown as Figure 13.

Figure 13. Height-time curve, showing ballast control action.

Since the rate switch is much more delicate than the displacement switch, safety considerations have caused the combined control to be supplemented by a pure displacement switch control. In this, the conducting segment of the pressure modulator is divided, and only a limited pressure height range (set for desired floating level) is controlled by both switches in series. If the rate switch is damaged at launching (by spilling some of its electrolyte, for instance) or in flight (perhaps by evaporation of the electrolyte) and the balloon descends, simple displacement control becomes effect when the high pressure lower altitude) segment of the conductor is touched by the pres-

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Report, cited by the archive. The PDF is mirrored here; the original link is under it. The text was read from the page images by an OCR model; expect the odd misread word. 882 pages are in the text index: search them above, or from the library's search.