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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…
Temperature effects were discussed previously in this report. Those discussions on superheat and adiabatic temperature change will apply to the general equation. In general, temperature of the free air and lifting gas can be measured to a fair degree of accuracy.

Balloon volume at any time is a function of original full balloon volume plus the summation of all the changes in volume due to pressure and temperature changes and loss of lifting gas. It will also be affected by loss or gain of air by the balloon through diffusion and intake of air through the appendix. The nonextensible balloon will have a maximum volume and thus any changes tending to increase the gas volume to a value greater than the balloon volume will result in a valving of the excess lifting gas into the air, or (in the case of a balloon which will carry internal pressure) a pressure increase of the lifting gas.

It is for this reason that a non-extensible balloon is said to be in a state of stable equilibrium in a direction of greater altitude when it is full. However, in a direction of lesser altitude, and with the case of a partially full floating balloon, the system is in a state of neutral equilibrium.

Composition of the lifting gas will change due to contamination of the lifting gas by the entry of air into the balloon, either by the flow of air through the appendix opening or by diffusion of air into the balloon. We may then modify our term for density of the lifting gas to include a term for the pure gas and a term for the contaminating air. Using the method of partial volumes, we may equate the density of the lifting gas at any time by:

where:

$$
\rho_ {g} = \frac {P _ {g}}{V _ {b} T _ {g}} \left(\frac {V _ {p}}{R _ {p}} + \frac {V _ {a}}{R _ {a}}\right)
$$

$ P_{g} $ pressure of the lifting gas

$ V_{b} $ = total lifting gas volume

$ V_{\mathbf{p}} $ volume of pure lifting gas in balloon

$ V_{\sigma} $ volume of air in balloon

$ R_{g}= $ specific gas constant of pure lifting gas

$ R_{a} $ specific gas constant of air

Then, calling $ \frac{V_{p}}{V_{b}}=x_{p} $ and $ \frac{V_{a}}{V_{b}}=x_{a} $ (here we see that since

$ V_{p}+V_{a}=V_{b}, $ $ x_{p}+x_{a}=1 $ we may equate:

$$
P _ {g} = \frac {P _ {g}}{T g} \left(\frac {x _ {p}}{R _ {p}} + \frac {x _ {a}}{R _ {a}}\right)
$$

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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.