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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. 39 …An advance ground team, led by Albert P. Cray, preceded the NYU group to Alamogordo Army…
  • p. 96 …OSI also developed an advanced Narcotics Investigations Course designed to teach the latest technics in combatting…
  • p. 174 …Dr Crary and Dr Peoples were the advance people and scientific monitors for our project. Dr…
  • p. 247 …Spilly was a consultant, and even in his advancing age he was still an enormous source…
  • p. 273 …the advance party of the balloon group arrived by B-17. $ ^{21} $ On May 29, the…
  • p. 617 …in advance of balloon release and a second notice will be filed at the time of…
  • p. 618 …Upon attaining the desired altitude, the auxiliary lifting balloons will be released from the main balloon…
  • p. 694 …in advance of balloon release and a second notice will be filed at the time of…
  • p. 695 (1) The type balloon to be used in this phase of the project will be a…
9 = the acceleration of gravity (ft./sec. $ ^{2} $ )

$ A_{0} $ area of the opening (ft.2)

h = head of fluid causing flow (ft.)

since $ h=\frac{1 4 4 \Delta p}{d_{q}} $ , we have:

$$
\Delta p = \frac {d g}{2 8 8 g} \left(\frac {1}{C _ {d} A _ {a}} \cdot \frac {d V}{d t}\right) ^ {2} \quad p s i
$$

where $ d_{g} $ is density of the lifting gas (1b./ft. $ ^{3} $ ).

From equation (7) we have:

$$
\frac {d V}{d t} = \frac {d z}{d t} \frac {V}{2 7 8 0 0} f t ^ {3} / \sec
$$

therefore:

$$
\Delta p = \frac {d g}{2 8 8 g} \left(\frac {1}{C _ {d} A _ {a}} \frac {d z}{d t} \cdot \frac {V}{2 7 8 0 0}\right) ^ {2}
$$

psi

Comparing equations (10) and (13) we see that if the equations are equal:

$$
\frac {1}{2 8 8 g C _ {d} ^ {2}} = \frac {1 4 . 7}{1 3 3 3 ^ {2} d _ {a 0}}
$$

If we let $ C_{d}=.975 $ , a reasonable value for the relatively low velocity flow of gas through the appendix, we have:

$$
\frac {1}{2 8 8 g C _ {d} ^ {2}} = 1 1 3. 5 \times 1 0 ^ {- 6} f t - \sec^ {2} / \ln^ {2}
$$

$$
\frac {1 4 . 7}{1 3 3 3 ^ {2} d _ {a 0}} = 1 1 4. 8 \times 1 0 ^ {- 6} f t - \sec^ {2} / \mathrm {i n} ^ {2}
$$

Therefore, the equations (10) and (13) are equal and interchangeable.

It may be noted from equations (10) and (13) that for any given balloon, appendix area and balloon volume are fixed, and the related variables are lifting gas density, rate of rise, and allowable back pressure. For any given allowable back pressure greater rates of rise are allowable at higher altitudes (where $ \mathbf{d}_{g} $ is lower).

Once a floating altitude has been decided upon or it has been decided to carry a given load as part of the balloon system, we can find a maximum allowable rate of rise. We must consider

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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.