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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…
in the preceding section on diffusion and leakage the appendix opening should be small. It can be seen that as we make one of our conditions better, we must sacrifice at least one of the others. Therefore, balloons must be designed compromising rate of rise, balloon thickness, and appendix opening. Methods of decreasing the appendix opening, except during the valving of lifting gas, are discussed in other sections of this technical report. In general they consist of means of applying a delicate relief valve, capable of opening to a large area with application of only slight internal pressure, and also closing tight upon release of this internal pressure.

## G. A General Equation of Motion

If we collect and relate the variables incidental to balloon flight, we may form a general equation of motion. This is most easily expressed in terms of forces acting upon the balloon system. We may equate an acceleration term plus a drag or friction term against term to include all other forces:

$$
m D ^ {2} z + n (D z) ^ {2} = \sum F
$$

This is a differential equation of a type common in mechanical vibration problems, and solution for the variable z would not be difficult if relationships of the many variables included in the the terms n and $ \sum F $ were simple. However, the complexity of the balloon system introduces many terms as parts of n and $ \sum F $ .

We shall first state the more complex form of equation (1) above and then attempt to explain the variables included in each part of the equation. As will be shown, it is extremely difficult to find a complete solution of the equation since many of the variables are in themselves extremely complex and at this time incapable of accurate solution. Therefore, our discussion will be more of a qualitative rather than a quantitative nature.

The general force equation is:

$$
\frac {W}{g} D ^ {2} z + C \frac {\rho}{2} A (D z) ^ {2} = V _ {b} \left(\rho_ {a} - \rho_ {g}\right) - W \pm F _ {a t m}
$$

The force due to acceleration $ F_{A}=\frac{W}{g} D^{2} z $ where:

W = weight of the balloon system

g = acceleration of gravity

$ D^{2} z= $ acceleration of the balloon system (An acceleration in the direction of greater altitude is considered positive.)

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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.