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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. 193 …overhead and followed the balloons out to sea. I have no idea about the results that…
  • p. 200 …the regular 334 that we had at sea level. From that they could deduce the temperature…
  • p. 243 …actually located on the jurisdictional lines between Sea Girt and Springlake, New Jersey. It was an…
  • p. 244 …The Sea Girt Inn? A: Exactly. That's where John had his office, and I was…
  • p. 320 …alone is about 24,000 miles at sea level, and about 4500 miles at 45,000…
  • p. 325 …twenty-five (25) feet at their largest sea-level diameter. The sonic unit was a combination…
  • p. 378 …per hour when one-fifth inflated at sea level). One other type of balloon which has…
  • p. 402 …Let us, then, compare the rate of leakage at any given altitude with leakage at sea…
  • p. 404 …The leakage at any altitude may be expressed as a function of leakage at sea level…
  • p. 405 Comparing rate of leakage at 40,000 feet with leakage at sea level: $$ \frac {L _ {4…
  • p. 407 …If a 20-foot diameter balloon $ \frac{1}{1 0} $ full were tested at sea level…
  • p. 408 …At sea level this is equivalent to 5.32 gm/hr. for a 20-foot diameter…
  • p. 414 …Using the rules of subsonic aerodynamics, Picard suggests that air at sea level escaping at 1333…
  • p. 415 …air at sea level (lb./ft. $ ^{3} $ ) 14.7 = pressure of air at sea level (psi…
  • p. 432 …to about 20 millibars and increased to sea-level pressure at different temperatures. The most comprehensive…
  • p. 563 …The height above mean sea level as determined from pressure measurements used in this work with…
  • p. 644 …point at which the radiosonde reaches the sea surface. ## 2. Earlier attempts There have been numerous…
  • p. 645 …The balloons floated between the surface and 30,000 ft above sea level; those which reached…
  • p. 704 …Met Gifford who has 90' sea rescue boat this project is planning to use. Stayed at…
  • p. 719 …Worzel working on gravity at sea. Saw Geo Woollard and the Ryders. Woollard after Guggenheim fellowship…
  • p. 779 …the launching site is markedly different from sea level, a shift in this curve is needed…
  • p. 817 …balloon at all times with respect to sea level. On this curve also it is customary…
  • p. 825 …The height above mean sea level as determined from pressure measurements used in this work with…
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.