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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.

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 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.