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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. 29 …Since 1978-1980, other UFO researchers, most notably Donald Schmitt and Kevin Randle, claim to have…
  • p. 31 …Randle and Donald Schmitt; The Truth About the UFO Crash at Roswell (1994), also by Randle…
  • p. 159 …I have reviewed the pictures in the 1991 Book by Randle and Schmitt on the UFO…
  • p. 168 …It had been alleged in a number ofbooks, including the one by Randle and Schmitt, that…
  • p. 170 …I went through and pulled out wherever, in this book UFO Crash at Roswell by Randle…
  • p. 171 …From the very start, when these clowns started hounding me, Randle and Schmitt, I told they…
  • p. 176 …He makes a number of claims that, at least Randle and Schmitt; and when I say…
  • p. 178 …risk injury to civiliaDs on the ground. Randle asked if he remembered my talk at aD…
  • p. 190 …Well, of course, Randle and Schmitt do claim that those people are out there and that…
  • p. 191 …Well, I got a perfect example of this with Randle and Schmitt. Randle is the outgoing…
  • p. 205 …On review of the photos in the Randle/Schmitt book, the material looks like one of…
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

About this file

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.