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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…
To use the first of these principles it is possible to main- tain a condition of buoyancy by at least the following two me- methods: (1) dropping a part of the load, as ballast, to match the loss of lifting gas which occurs as a result of diffusion and leakage; (2) replacement of the lifting gas by evaporation from a reservoir of liquified helium or hydrogen. Of these two methods, ballast dropping is most satisfactory from the consideration of simplicity of control and safety of personnel. While the use of liquid helium is theoretically more efficient, the amount and com- plexity of control equipment adds much to the cost and also the weight of air-borne equipment.

The development of non-elastic balloons which can withstand high internal pressure was investigated. Two designs which compromise extreme cost (required for balloons of high internal pressure) with small wall strength, hence small super pressure, were tested.

At first, attempts were made to control balloon performance by using buoyancy-load balance techniques with elastic balloons, but the difficulties which were experienced resulted in the development of a third principle of operation combining a non-extensible balloon with a system of controls which can be applied either to a freely expanding balloon or to a balloon of fixed volume.

## III. METHODS OF ATTACK

The work on the development of controlled-altitude balloons may be divided into three phases, each one identified by the type of balloon which was used. Concurrent with the balloon development was the design and testing of control equipment required to maintain the balloon at specific altitudes. Some of the equipment instrumentation was used on more than one kind of balloon, but in general the problems and methods of attack are identified with one of the three types of balloons.

## A. Rubber Balloons

Following the example of Clarke and Korff, assemblies of neoprene rubber balloons were first considered. Using these freely expanding balloons it was necessary to balance the load to be lifted with the buoyancy given by an integral number of balloons. One or more accessory balloons were attached to the assembly to provide lifting force to carry the train aloft. With the gear at a predetermined altitude, the lifting balloons were cut loose from the train by a pressure-activated switch, leaving the equipment at floating level, more or less exactly balanced. Since there is no inherent stability in an extensible balloon, any existing unbalance will cause the train to rise or fall indefinitely until the balloon reaches

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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.