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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. 8 …Computer Specialist, Office of the Secretary of the Air Force, Pentagon; George Cully, Historian, 81st Training…
  • p. 20 …FOR THE SECRETARY OF THE AIR FORCE FROM: SAF/AAZ 1720 Air Force Pentagon Washington, DC…
  • p. 56 …SAF/FMPF, Room 4C228, Pentagon SUBJECT: Central Point of Contact, GAO Code 701034 2. You will…
  • p. 58 # DEPARTMENT OF THE AIR FORCE WASHINGTON DC 20330-1000 OFFICE OF THE SECRETARY MEMORANDUM FOR DISTRIBUTION…
  • p. 59 …SAF/AAZ 1720 Air Force Pentagon Washington DC 20330-1720 SUBJECT: GAO Review on Records Management…
  • p. 75 …HQ USAF/XOWP 1490 Air Force Pentagon Washington DC 20330-1490 SUBJECT: GAO Review on Records…
  • p. 77 10 March 1994 SAF/AAIQ 1610 Air Force Pentagon Washington, DC 20330-1610 MEMORANDUM FOR SAF…
  • p. 78 …They noted that the histories for the 509th Bomb Group and Wing for Roswell Army Air…
  • p. 145 …the Pentagon if he had a problem with that he could take it up with the…
  • p. 185 …Perhaps you have it from the Pentagon files already, from the AG files. ## Q: We have…
  • p. 246 …Following that, I spent more than three years on the Air Staff in the Pentagon. Q…
  • p. 268 …Force Pentagon Washington, DC 20330-1720 SUBJECT: Report of Findings on Balloon Research The following report…
in high altitudes, since it freezes below -80 $ ^{\circ} \mathrm{C} $ and will flow readily at low temperatures. Also, this fluid will absorb only a very slight amount of water which might freeze aloft.

Basically three different principles have been used in the control of ballast flow. The first of these is calculated constant flow; the second is displacement-switch control; and the third is rate-of-ascent switch control.

## (1) Constant Flow

In the simplest of the control systems, liquid ballast is allowed to flow continuously through an orifice (Figure 8) at a predetermined rate. This rate is set to slightly exceed the expected loss of lift of the balloon due to leakage and diffusion. If this method is successfully used, the balloon stays full because the gas remaining in it has less load to support. Therefore, the balloon will rise slowly as ballast is dropped, maintaining equilibrium between the buoyancy and the load. In the General Mills 20-foot balloon, for example, diffusion losses are about 200 grams per hour at altitudes near 40,000 feet. The balloon at its ceiling of 40,000 feet with a 26-kilogram payload rises about 700 feet with each kilogram of ballast dropped. This means that such a balloon using this constant-flow type control will float at a "ceiling" which rises at the rate of about 140 feet per hour. Constant flow was first obtained by use of the manual ballast valve shown in Figure 9. Due to excessive clogging of this valve, caused by its annular ring opening, gate-type valves were tested, and finally the use of

Figure 8. Orifice for fixed-rate ballast flow.

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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.