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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…
its bursting diameter, the gear strikes the ground, or corrective action is taken. Even if the extremely critical balance is initially achieved, there will be unbalance occasioned by (1) bursting of balloons due to deterioration in the sunlight, (2) diffusion of lifting gas from the balloons, (3) loss or gain of buoyancy when temperature inside the balloon changes with respect to the ambient air temperature. This will result initially from radiative differences, and after an amount of difference (superheat) has been established, changes in ventilation will cause changes in buoyancy.

Two methods of attaching the payload to the clusters of rubber balloons were tried. In the first of these (Figure 3) a long load line was used, and short lines led from it to the individual balloons. The length of such arrays was as much as 800 feet, and this size made them difficult to launch. The single load ring array, seen in Figure 4, proved to be much easier to handle and is recommended for cluster launchings. During ascent each of the balloons in such an array ride separated from each other and no rubbing or chafing has been observed.

The controls which were associated with this balloon system were crude and, in general, ineffective. They included (1) cutting off balloons as the buoyancy became excessive and a preset altitude extreme was passed, and (2) releasing part of the load in the form of solid or liquid ballast whenever descent occurred. The sensitivity of these elastic balloons makes it difficult to control their altitude with any system of controls, and as controls were developed it was found more practical to change from freely expanding balloons to non-extensible cells not made of neoprene. The tendency of neoprene to decay within a few hours when exposed to sunlight was the most cogent argument against doing more work on altitude controls to be used with such a system.

## B. Plastic Balloons

The next attempts to control the altitude of a balloon vehicle were made using non-extensible plastic cells, with an open bottom to prevent rupture when expansion of the lifting gas is excessive. With a fixed maximum volume, such a system has inherent vertical instability in only one direction. When full, there is a pressure altitude above which a given load will not be carried. The instability of such a system is found only when an unbalanced downward force exists. The development of controls and films for balloon material proceeded concurrently, but the choice of a non-extensible plastic film was made before the system of control was perfected.

The properties which were given most consideration in the selection of fabric include (1) availability and cost, (2) ease of fabrication and (3) satisfactory chemical and physical properties. Pri-

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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.