Documents / Report

The Roswell Report: Fact vs. Fiction in the New Mexico Desert

USAF / The Black Vault · 1995 · 882 pages · text by GLM-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. 397 …R _ {g} T _ {g _ {2}}} - \frac {1}{R _ {g} T _ {1}}\right) \\ = \frac {V _ {p}}{R…
  • p. 398 …R _ {g} T _ {2}}\right) - \left(\frac {p}{R _ {a} T _ {2}} - \frac {p}{R _ {g…
  • p. 399 …left(\frac {1}{R _ {a}} - \frac {1}{R _ {g}}\right)} $$ (9) $$ = \frac {1}{1 - B} \left…
  • p. 420 …F = $ V_{b}\left(\frac{P_{g}}{R_{a}T_{a}}-\frac{P_{g}}{R_{g…
  • p. 421 …V_{\sigma} $ volume of air in balloon $ R_{g}= $ specific gas constant of pure lifting gas…

Read from the scan by GLM-OCR; expect the odd misread word.

We see that the maximum allowable $ \mathrm{(d p / d z)}_{\mathrm{q}} $ (1-B) for a 30' diameter, .001" thick polyethylene balloon is $ 2 5 6 \times 1 0^{-3} \mathrm{p s i / f t} $ . Dividing by (1-B) we have the maximum allowable:

$$
\begin{array}{l} \left(\mathrm {d p} / \mathrm {d z}\right) _ {a} = \frac {2 5 6 \times 1 0 ^ {- 3}}{1 - . 1 3 8} = . 3 0 0 \times 1 0 \mathrm {p s i} / \mathrm {f t} ^ {- 3} \\ = 2 0. 7 \times 1 0 ^ {- 3} \mathrm {m b} / \mathrm {f t} \\ \end{array}
$$

This is comparable to an altitude of 18,300 ft. or a gross buoyancy of 450 lb., the maximum allowable inflation of a 30' diameter, .001" thick polyethylene balloon from the standpoint of pressure distribution.

In order to determine mathematically the point of failure due to pressure distribution we may use equations (3) and (5) and their derivatives:

$$
\Delta p _ {z} = \Delta z \left(\frac {d p}{d z}\right) _ {a i r} (1 - B)
$$

$$
\Delta p _ {z} = \frac {4 S f t}{2 \left(D \Delta Z - \Delta Z ^ {2}\right) ^ {1 / 2}}
$$

at the point of tangency of these curves (T in Figure 26):

$$
\Delta p _ {T 3} = \Delta p _ {T 5} \quad \text {a n d} \quad \left(\frac {d p}{d z}\right) _ {T 3} = \left(\frac {d p}{d z}\right) _ {T 5}
$$

in equation (5), making $ \frac{4311}{2}=K $ and in equation (3), making $ (dp/dZ)_{0}(1-B)=m $ , the slope of the line $ \Delta p_{z}=\Delta Z\cdot m $ we have:

(5a)

$$
\Delta p _ {z} = \frac {K}{(D \Delta z - \Delta z ^ {2}) ^ {1 / 2}}
$$

and:

(3a)

$$
\Delta p _ {z} = m \Delta z
$$

differentiating with respect to z :

(5b)

$$
\frac {d p}{d z} = - \frac {K}{2} \frac {(D - 2 \Delta Z)}{(D \Delta Z - \Delta Z ^ {2})}
$$

$$
\frac {d p}{d z} = m
$$

(3b)

Cited by

Cases discussed

About this file

Report, cited by the archive. The PDF is mirrored here; the original link is above. The text was read from the page images by GLM-OCR; expect the odd misread word. 882 pages are in the text index: search them above, or from the library's search.