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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. 190 …Well, Boford was Navy, that was the Navy... Q: Like taking a Pi Ball reading now…
  • p. 191 …fabricate balloons for us. During that period we heard of the Navy project that was going…
  • p. 207 …But were any of those used as precursors to Mogul or... A: None whatsoever. That was…
  • p. 270 …Ewing had conducted considerable research for the Navy during World War II, studying, among other things…
  • p. 323 …f) Measurements of actual sound channel transmission using a small stratosphere balloon carrying sound receivers and…
  • p. 657 …At the present time this company cannot supply us with balloons until Navy clearance is obtained…
  • p. 693 …for six hours using a non-extensible envelope with the addition of a ballast valve to…
  • p. 704 …Met Gifford who has 90' sea rescue boat this project is planning to use. Stayed at…
  • p. 705 …Wyckoff, Hungerfield, Vaux and myself regarding Navy participation with us in Crossroads. Captain Kellogg of Weather…
  • p. 718 …Schneider up with O'Day to check use as NYU station. Alamoggrdo crew helped get helium…
The equation for the force due to buoyancy will then become:

$$
F _ {b} = V _ {b} \left[ \frac {P _ {a}}{R _ {a} T _ {a}} - \frac {P _ {a}}{T _ {g}} \left(\frac {x _ {p}}{R _ {p}} + \frac {x _ {a}}{R _ {a}}\right) \right]
$$

If the balloon is of the type that will carry no internal pressure $ p_{a}=p_{g} $ , and we may state that:

$$
F _ {b} = V _ {b} p _ {a} \left[ \frac {1}{R a T a} - \frac {1}{T g} \left(\frac {x _ {p}}{R p} + \frac {x _ {a}}{R a}\right) \right]
$$

Discussions of the contamination of the lifting gas are included under the section on "Diffusion and Leakage of Lifting Gas" of this report.

The force due to the weight of the system $ F_{W}=W $ The weight of the balloon system at any time is a function of the original weight of the system plus the change of weight of the system. This change in the weight of the system is caused by the loss of ballast and the weight of the system at any time ( $ \uparrow $ ):

$$
W _ {t} = W _ {0} - \sum_ {t = 0} ^ {t} \Delta W _ {b}
$$

where:

$$
W _ {0} = \text {t h e o r i g i n a l w e i g h t o f t h e s y s t e m}
$$

$ \sum_{t=0}^{r} \Delta W_{b} = $ the sum of all the losses of ballast from time at which $ W=W_{0} $ until the time $ \dagger $

The value of the term $ \sum_{t=0}^{\infty} \Delta W_{b} $ depends on the type of ballast control. With no ballast:

$$
\sum_ {\mathrm {t} = 0} ^ {+} \Delta W _ {\mathrm {b}} = 0 \quad \mathrm {a n d} \quad W _ {\dagger} = W _ {0}
$$

If a constant ballast flow is used:

$$
\sum_ {t = 0} ^ {1} \Delta W _ {b} = \frac {d W}{d t} t
$$

where:

$ \frac{dW}{dt}=rate of ballast flow $

$ \uparrow $ = elapsed time from $ \uparrow = 0 $ to $ \uparrow = \uparrow $

If a practical fixed opening type or ballast control is used:

where:

$$
\sum_ {t = 0} ^ {+} \Delta W _ {b} = f (t, h, \mu_ {b}, \rho_ {b}, A)
$$

↑ = time

h = head of ballast above opening

$ \mu_{b}= $ viscosity of ballast fluid

$ P_{b} $ density of ballast fluid

A = area of opening

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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.