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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 …Computer Specialist, Office of the Secretary of the Air Force, Pentagon; George Cully, Historian, 81st Training…
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  • p. 268 …Force Pentagon Washington, DC 20330-1720 SUBJECT: Report of Findings on Balloon Research The following report…
This effect adds to the stability of stratospheric balloon flights. If a system in equilibrium in the stratosphere were to lose lift and descend, the compression of the gas would cause an increase of the lifting gas temperature relative to the air temperature, causing a decrease in unbalance.

Similarly, an initial unbalance causing rise of the system would cause relative cooling of the lifting gas and thus again decrease the unbalance. Hence, the rate of rise or descent in the stratosphere will be limited by the rate of heat exchange due to conduction and radiation, which will counteract this effect of adiabatic heating or cooling.

Empirical evidence indicates that there is a great deal more stability in a stratospheric balloon system than in a similar system floating in the troposphere. This "adiabatic stability" is a principal reason for better performance of stratosphere flights.

## E. Diffusion and Leakage of Lifting Gas

The lifting gas of a balloon can be lost by:

leakage through small holes in the fabric or film; solution, migration and evaporation through fabric or film; true molecular diffusion through openings, such as the appendix opening.

## (1) Leakage

Volumetric flow, Q, of a gas through any given opening in the balloon surface may be evaluated as a function of the area of the opening, A; the pressure head causing the flow, h and a coefficient of leakage, $ C_{d} $

$$
Q = C _ {d} A \sqrt {2 g h}
$$

where g is the acceleration due to gravity

It would be difficult to evaluate the amount and area of holes in the balloon surface. Let us, then, compare the rate of leakage at any given altitude with leakage at sea level, rather than attempting to evaluate the leakage at a given altitude.

First we shall compare the rate of leakage of a full balloon at any given altitude with leakage of a full balloon at sea level. Let us assume that the area of any opening in the surface of the balloon does not vary with altitude and that the coefficient of leakage is constant. Thus:

$$
Q \sim \sqrt {h}
$$

where h is pressure head in feet of lifting gas

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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.