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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. 23 …Air Force Historical Research Agency (AFHRA), Maxwell Air Force Base (AFB), AL, the Air Force Safety…
  • p. 28 …What Air Force researchers did do, however, was to search for records still under Air Force…
  • p. 47 …Much of the speculation stems from claims by William Haut, a former Air Force public affairs…
  • p. 65 …On orders from the base commander, Col. William Blanchard, the Public Information Officer, Walter G. Haut…
  • p. 135 …That actually came, I think, in September when the Air Force first stated. You were one…
  • p. 277 …Commander, Eighth Air Force. General Ramey personally inspected the "disc," became skeptical, and summoned the base
$$
\frac {\Delta L}{L _ {1}} = \frac {B}{1 - B} \left(\frac {T _ {g _ {2}} - T _ {1}}{T _ {g _ {2}}}\right)
$$

or, for small temperature differences, we have:

(6)

$$
\frac {\Delta L}{L} = \frac {B}{1 - B} \left(\frac {\Delta T}{T}\right)
$$

With increasing temperatures, there will be an unbalance in the direction of greater altitude. While climbing to a greater altitude the balloon will valve gas and come to equilibrium at a new level. Thus the effect of gain of superheat with a full nonextensible balloon will be a slight increase of altitude.

Investigating the case where an initial amount of superheat is lost:

$$
\Delta L = V _ {2} \left(d _ {a _ {2}} - d _ {g _ {2}}\right) - V _ {1} \left(d _ {a _ {1}} - d _ {g _ {1}}\right)
$$

and since the balloon volume will decrease with cooling of the lifting gas:

$$
V _ {2} = V _ {1} \frac {T g _ {2}}{T g _ {1}}
$$

(assuming constant p)

Therefore, again making use of the assumptions that:

$$
P _ {a _ {1}} = P _ {a _ {2}} = P _ {g _ {1}} = P _ {g _ {2}} = P
$$

and:

$$
T g _ {2} = T a _ {1} = T a _ {2} = T _ {2}
$$

Combining equation (2) and equation (7), we have:

$$
\begin{array}{l} \Delta L = V _ {1} \left[ \frac {T _ {2}}{T _ {g _ {1}}} \left(\frac {p}{R _ {a} T _ {2}} - \frac {p}{R _ {g} T _ {2}}\right) - \left(\frac {p}{R _ {a} T _ {2}} - \frac {p}{R _ {g} T _ {g}}\right) \right] \\ = V _ {1} \left(\frac {p}{R _ {a} T _ {g _ {1}}} - \frac {p}{R _ {g} T _ {g _ {1}}} - \frac {p}{R _ {a} T _ {2}} + \frac {p}{R _ {g} T _ {g _ {1}}}\right) \\ \end{array}
$$

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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.