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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. 8 …David Thurston, Secretary of the Air Force Public Affairs Office; Dr. Saxson and Betsy Hudon of…
  • p. 30 …XOW, Directorate of Weather (g) added later The Air Force Office of Special Investigations (AFOSI) In…
  • p. 68 …Ruppelt was the UFO study project officer from 1951-1953 and he investigated a series of…
  • p. 95 …These records contain documents on investigative policy and Air Force Office of Special Investigation reports of…
  • p. 262 …of criminal activity which may require investigative action by commanders, supervisor, security police, AFOSI special agents…
  • p. 263 …Rogan who advised me, he was assisting in an investigation at the behest of the Secretary…
  • p. 314 …Lt Colonel Maas was assigned as Base Weather Officer and as head of the E&A…
the equation 2500 ft. $ ^{3} / 1 \mathrm{b}. $ mol = ae $ ^{50 b} $ where 50 is the expression for altitude in thousands of feet. Similarly, at 70,000 feet, $ 6 4 5 0=a e^{7 0 b}, $ and by solving to eliminate a, we find $ 2. 5 8=e^{2 0 b} $ or 20b = .95, and the constant b is equal to .0475. Thus, the equation may be written:

(3)

$$
y = a e ^ {. 0 4 7 5 z}
$$

y was originally defined as the molar volume, equal (for 98% helium) to:

$$
\frac {\text {Balloon Volume} \times 2 4 . 4}{\text {Gross Load}} = \frac {K}{W}
$$

In turn, $ \frac{K}{W}=a e^{-0. 4 7 5 z} $ , where z is the expression for altitude in thousands of feet. From this relationship, we may solve for W, the gross load.

(4)

$$
W = \frac {K}{a} e ^ {- 0. 4 7 5 z}
$$

(5)

$$
\ln \left(\frac {W a}{K}\right) = - 0. 4 7 5 z
$$

or:

(6)

$$
\ln W + \ln \frac {a}{K} = - 0. 4 7 5 z
$$

Differentiating with respect to W:

$$
\frac {d z}{d W} = - \frac {2 1 . 0 5 2}{W} \frac {f t}{l b}
$$

where W is gross load in lb.

We see that the value of the constant a is unimportant here, and the expression is independent of balloon volume, as long as it does not vary with time. Included is the assumption that over a short period of time buoyancy of lifting gas does not change.

Thus, we have an expression for A, the altitude sensitivity, which is valid between 40,000 and 105,000 feet. Similarly, it is possible to evaluate altitude sensitivity for operation between O and 30,000 feet. A in this range is equal to 31,400 ft./lb.

A plot of altitude sensitivity against load is shown on page 109 of the "Operations" section (Part II of this technical report).

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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.