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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. 28 …Evidence in Search of Proof" (1985) by Moore; The UFO Crash at Roswell (1991) by Kevin…
  • p. 33 …There were no ancillary records in Air Force files to indicate the potential existence of such…
  • p. 66 …All of this organization's UFO study files were transferred to the National Archives and made…
  • p. 68 …These primary documents should have been part of this organization's UFO study files and currently…
  • p. 81 …On 2 March 1994, Inquiries Branch staff developed a list of possible file locations which might…
  • p. 83 …ROSWELL UFO UFOS UNIDENTIFIED FLYING OBJECTS WEATHER BALLOON WEATHER BALLOONS The IRIS search produced no documents…
  • p. 95 …These files contain policy guidance and AFOSI District reports of investigation concerning UFOs (filed primarily by…
  • p. 96 …These phenomena, later termed unidentified flying objects or UFOs, had been sighted with some frequency in…
  • p. 237 …He appeared to want to substantiate the existence of the UFO incident as a UFO. I…
When the system again descends to 25,000, the pen arm comes into contact with the commutator contact and an electrical circuit is closed through a squib in the load line. The load line is cut and the load on the system falls six to eight feet before being caught by a supplementary load line. During this fall a rip line pulls a hole one foot long in the side of the balloon and the system descends using the partially inflated balloon to hold the rate of descent to approximately 1200 ft/minute. This system has been used successfully in over 100 flights.

A drawing of the rip assembly is shown as Fig. 13. The cannon and squib to cut the load line are shown as Fig. 14.

Fig.13 Balloon Rip Assembly

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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.