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The Roswell Report: Fact vs. Fiction in the New Mexico Desert

USAF / The Black Vault · 1995 · 882 pages · text by OCR

The Roswell Report: Fact versus Fiction in the New Mexico Desert was published by Headquarters United States Air Force in 1995. The Black Vault distributes this copy. It reproduces the report by Col. Richard L. Weaver and the synopsis by 1st Lt. James McAndrew, both written after a General Accounting Office inquiry requested by Representative Steven Schiff. The Air Force search found no evidence of an extraterrestrial craft or crew. It concluded that the Roswell debris most likely came from NYU Flight No. 4, a Project MOGUL balloon train.

  • p. 190 …Well, Boford was Navy, that was the Navy... Q: Like taking a Pi Ball reading now…
  • p. 191 …fabricate balloons for us. During that period we heard of the Navy project that was going…
  • p. 207 …But were any of those used as precursors to Mogul or... A: None whatsoever. That was…
  • p. 270 …Ewing had conducted considerable research for the Navy during World War II, studying, among other things…
  • p. 323 …f) Measurements of actual sound channel transmission using a small stratosphere balloon carrying sound receivers and…
  • p. 657 …At the present time this company cannot supply us with balloons until Navy clearance is obtained…
  • p. 693 …for six hours using a non-extensible envelope with the addition of a ballast valve to…
  • p. 704 …Met Gifford who has 90' sea rescue boat this project is planning to use. Stayed at…
  • p. 705 …Wyckoff, Hungerfield, Vaux and myself regarding Navy participation with us in Crossroads. Captain Kellogg of Weather…
  • p. 718 …Schneider up with O'Day to check use as NYU station. Alamoggrdo crew helped get helium…
## Flight 110: Released from Alamogordo, New Mexico, 0649 MST, February 11, 1949 Recovered at Kershaw, South Carolina

This flight had as its main objectives the testing of a Winzen Research Inc. .0015", 20-foot polyethylene balloon, and further testing of the combination ballast control-displacement switch and rate-of-ascent switch. Following the initial ascent of this flight, a slow descent resulted from loss of lifting gas. Three hours were required for a descent of 2000 feet to the pressure where ballast flow was begun. This and the general flight pattern indicate the satisfactory nature of this Winzen Research Inc. balloon. After ballast started, the valve stuck and a constant flow at 1800 grams per hour followed. The rising ceiling seen in Figure 56 is the typical flight pattern for a balloon whose load is being steadily decreased at a rate in excess of the loss of buoyancy.

Figure 56

On this flight all three of the receiving stations positioned along the expected path were able to receive and record the pressure and ballast signal. No temperature equipment was flown.

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Report, cited by the archive. The PDF is mirrored here; the original link is under it. The text was read from the page images by an OCR model; expect the odd misread word. 882 pages are in the text index: search them above, or from the library's search.