Documents / FOIA release

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. 539 …Too muoh weight was lost in this action, and the train rose until aome of the…
  • p. 540 …Train, Flight 10 The balloon rose to about 16,000 teet MSL and dropped back to…
  • p. 554 …It will be seen that the balloon rose~ a ' .. --------- r- ....., ..:. Pon"'m j"'.,.._" k '~I I…
  • p. 572 …obtained, but during this time the balloon rose with predicted speed (500 feet per minute) nearly…
  • p. 585 …On the other hand, the balloon rose extremely slowly and may have taken in air to…
  • p. 665 …In flight 7, however, the cluster rose till the lifters were cut off, descended until sufficient…
  • p. 739 …As a result, the cluster rose to ceiling and stayed at this altitude for a short…
  • p. 786 s4cond cluster flight, provision was also made to release balloons if the train rose above 40…
to the automatic ballast valve system, a. tixed-tlow needle valw was set
to dischar~ ballast slightly in •xcess of the expected loss. Both 1ystems
tailed to keep the balloon afloat, and a. 1low de1cent tro.m ita maximum alti-
tude of 14,000 feet MSL re1ulted. 1he expected altitude of 38,000 feet
was not reached, and this is believed to be due to mixing of the air with
the lifting gas during rising. The bottom of tl'le balloon was open with
no protecting skirt or valve to keep out air. Since the thin fabric would
rupture with an internal pressure of 0.017 psi, some form of skirt or ex-
ternal appendix was suggested for future flights.
Radio reception with the 3 me transmitter was excellent and tar sur-
passed the performance of either the 72 mo· or 394 me transmitters which were
also flown.
Because of the low elevation angle of the transmitter, the single SCR-658
radio direction-finding equipment was not of much use for positioning.
Tracking by aircraft was satisfactory throughout the flight.
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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.