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. 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-
signals may be arranged so as to consume a very
small portion of -transmission time.
D. The duration of radio reception and of positioning data
may be greatly extended by appropriately equipped aircraft.
It is intended to utilize a B-17 with top~ounted radar to
search above the plane for tracking. Depending upon the
noise-level encountered, it may be possible to acquire
pressure data with a receiver in the plane. It may be
necessary to provide at least two aircraft for continuous
reception over long periods.
2. It is very desirable that the simplified ligbt-weigbt ballast
control system for flights of less than 24 hours' duration be
perfected. The elaborate ballast assembly with the automatic
ballast valve will not be needed for the many contemplated
flights which will be made with a useful life of less than
eight hours. A lower-capacity reservoir with manual ballast
valve and filter provides a light-weight, inexpensive unit.
Tests are now being conducted to find the best design for these
components.
3. In order to float a balloon at a pre-selected maximum altitude
it is necessary to supplement the variation-of-ballast with a new
height control system.
A. With a given balloon, and given total load, it is
possible to forecast the maximum height. (See Section
III for the computation.) If various ~Aximum heights
are desired, this maximum height may be varied by
varyin~ the total load, or varying the bouyancy of
the balloon through variation in balloon volume.
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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.