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-
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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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.