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roswell

Office of the Secretary of Defense · 993 pages · text from the file's own layer

The Roswell Report: Fact versus Fiction in the New Mexico Desert was published in 1995 by Headquarters United States Air Force. It was written in response to Representative Steven H. Schiff's request and a General Accounting Office audit, and it contains Col. Richard L. Weaver's report and 1st Lt. James McAndrew's synopsis, along with attachments, appendices and photographs. The report says researchers found no evidence of an extraterrestrial craft or crew. It concludes that the 1947 debris came from a Project MOGUL balloon train.

  • p. 7 …Computer Specialist, Office of the Secretary of the Air Force, Pentagon; George Cully, Historian, 81st Training…
  • p. 21 …FOR THE SECRETARY OF THE AIR FORCE FROM: SAF/AAZ 1720 Air Force Pentagon Washington, DC…
  • p. 64 …SAF/FMPF, Room 4C228, Pentagon SUBJECT: Central Point of Contact., GAO Code 701034 l. CPC Richard…
  • p. 67 OF"F'1C£ 0~ THE SECRETARY DEPARTMENT OF THE AIR FORCE WASHINGTON DC 20330-1000 MEMORANDUM…
  • p. 68 OFF'ICE OF" TME SECRETA~Y DEPARTMENT OF THE AIR FORCE WASHINGTON DC 20330-1000 MEMORANDUM…
  • p. 89 DEPARTMENT OF THE AIR FORCE HEADQUARTERS UNITED STATES AIR FORCE 09 Mar94 MEMORANDUMFORSAF/AAZ ATIENTION: Lt…
  • p. 174 …the Pentagon if he had a problem with that he could take it up with the…
  • p. 220 …Perhaps you have it from the Pentagon files already, from the AG files. Q: We have…
  • p. 282 …Following that, I spent more than three years on the Air Staff in the Pentagon. Q…
  • p. 317 …Force Pentagon Washington, DC 20330-1720 SUBJECT: Report of Findings on Balloon Research The following report…
18.
When the system again descends to 2.5 11 ()(X), the pen arm comes into
contact ~iith 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. Dnring 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 f-'"/minute. This system
has been ,,sed successfully in .over 100 flights.
A drawing of the rip assembly is shown as FjP". 13. The cannon and
squib to cut the load line are shown as Fig. :t!i.
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Fig, lj
Balloon Hip Assembly

Cases discussed

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FOIA release, from the osd collection. The PDF is mirrored here; the original link is under it. 993 pages are in the text index: search them above, or from the library's search.