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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…
or sunset cuts off the superheat is so large that it is not possible to carry enough ballast to sustain the system under these conditions. On the other hand, the loss of buoyancy through a sealed-off Seyfang balloon at 4100 feet MSL is of the order of 50 grams per hour which is significantly less than the loss expected from a 20-foot, 1 mil polyethylene cell in flight conditions. (With the appendix aperture sealed, such a cell shows a loss of lift of about 40 grams per hour when one-fifth inflated at sea level).

One other type of balloon which has been used as a super-pressure balloon is the neoprene J2000 balloon of Dewey and Almy, surrounded by nylon cloth shroud. The rubber balloon normally would expand until it reached bursting diameter, but when enshrouded, it is limited to the volume of the shroud. The difficulties in launching and flying this balloon are not unusually great, but on each of the several tests which have been made to date improper handling has been a possible cause of the early rupture of the balloon. It is believed, however, that such a balloon is not especially suitable for long flights because of the deterioration which occurs in the neoprene in the presence of sunlight. Perhaps a shroud of material which would filter out the ultraviolet rays would protect and lengthen the life of such a balloon.

Despite the success of the Japanese silk or rice-paper balloons, which were constructed on a super-pressure principle, it is not believed practical at this time to develop a balloon of such strength that it would successfully withstand and retain pressure increases corresponding to the temperature changes from night to day as the superheat of absorbed sunlight is gained. The super-pressure with a neoprene-coated nylon balloon, for example, would be approximately 0.5 psi. That such a balloon could be built is unquestioned. The cost of production, however, appears at this time to be unwarranted.

## D. Altitude Controls

Beginning with the arrays of rubber balloons which were first used, various systems of dropping ballast, both solid and liquid, have been attempted with the aim of exactly compensating for the loss of buoyancy which is occasioned as the lifting gas diffuses or leaks through the balloon. On the early rubber balloons only rough incremental ballast dropping was empbyed. At that time it was decided not to use sand as ballast since most sand contains some water which may freeze while aloft. Further, it is easier to control the flow of a liquid ballast than it is to control sand particles. In the investigations for a suitable liquid ballast the petroleum product known commercially as Mobil Aero compass fluid was finally settled upon. These investigations included tests of cloud point, freezing point, and also density and viscosity over a large range of temperatures. The compass fluid is especially suitable for ballast work

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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.