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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. 8 …Computer Specialist, Office of the Secretary of the Air Force, Pentagon; George Cully, Historian, 81st Training…
  • p. 20 …FOR THE SECRETARY OF THE AIR FORCE FROM: SAF/AAZ 1720 Air Force Pentagon Washington, DC…
  • p. 56 …SAF/FMPF, Room 4C228, Pentagon SUBJECT: Central Point of Contact, GAO Code 701034 2. You will…
  • p. 58 # DEPARTMENT OF THE AIR FORCE WASHINGTON DC 20330-1000 OFFICE OF THE SECRETARY MEMORANDUM FOR DISTRIBUTION…
  • p. 59 …SAF/AAZ 1720 Air Force Pentagon Washington DC 20330-1720 SUBJECT: GAO Review on Records Management…
  • p. 75 …HQ USAF/XOWP 1490 Air Force Pentagon Washington DC 20330-1490 SUBJECT: GAO Review on Records…
  • p. 77 10 March 1994 SAF/AAIQ 1610 Air Force Pentagon Washington, DC 20330-1610 MEMORANDUM FOR SAF…
  • p. 78 …They noted that the histories for the 509th Bomb Group and Wing for Roswell Army Air…
  • p. 145 …the Pentagon if he had a problem with that he could take it up with the…
  • p. 185 …Perhaps you have it from the Pentagon files already, from the AG files. ## Q: We have…
  • p. 246 …Following that, I spent more than three years on the Air Staff in the Pentagon. Q…
  • p. 268 …Force Pentagon Washington, DC 20330-1720 SUBJECT: Report of Findings on Balloon Research The following report…
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.