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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. 439 …it desired) Payload in~trumentation 1 ea. banner, 3 1 x 61 Data sheets. Weight sheets…
  • p. 550 …When mounted above the 'cloth identification banner, this chute also acts to minimize rrwe.y and…
  • p. 663 …A banner may be seen in Figure 30.. White banners seem to be the most generally…
  • p. 664 Figure 30 General Mills 20 foot balloon in flight, showine; banner and other flight train components.
  • p. 726 …description --------- Line leneth .---------------------------- Banner description --------------------------Ballast assembly .. description ______,.. Ballast • • .. • • '" • Total Equipment l~eight. • • • • ' Gross Load • • ' • • • • {56)
  • p. 860 …cutter cannon • • • • • • • • • 26 15 , Detail drawing of banner • • • • • • • • • • • • • • • • 28 16 • Typical service flight train (complete) • • • • • • • •• 30…
  • p. 881 …These are: (l) a banner, (2) a drag parachute, and (3) safety-weights. The banner is…
  • p. 882 …6' 12' NYU BALLOON PROJECT 3' 6' BANNER ~~~ Date~ 5-19-48 ED 48-5 6…
  • p. 937 2 ea. Parachutes ML-132 1 ea. Banner. 3' x 6' 4 ea. Data sheets 4…
  • p. 938 …description.______________ Drag chute ---------------------------- Banner description --------------- ---------- Ballast assembly - description -----------~-- Ballast • • • • • • Total Equipment i'ieight • • ' • • • • • • Gross Load • • • • • • • • • • • -86-
In this study four flights were made to study conditiona
at altit11des of 45,000 and 6o,ooo f't. A clock timer
was set to cause release or ballast after the B,ystem
had :floated at the lower level for one hour. After
ballast was expended the timer caused release of the
ballast tank to further reduce the load on the systems •
A typical flight of this series is shown as Fig. 15.
Further detailc on this stud1 pave been given in reports
on "Neutron Intensity Study"~5J by this Research Division.
60,000
50,000 r-LEVEL
~
DESCENT)
., 40,000a
t:.,
.., 30,000
0
::::)
~ 20,000
~
0 0~----~----~~----~.----~.----~5----~6
Till£ AFTER RELEASE - HOURS
Fig. 15
"Two Level" Stepped Flight
23.

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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.