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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. 193 …overhead and followed the balloons out to sea. I have no idea about the results that…
  • p. 200 …the regular 334 that we had at sea level. From that they could deduce the temperature…
  • p. 243 …actually located on the jurisdictional lines between Sea Girt and Springlake, New Jersey. It was an…
  • p. 244 …The Sea Girt Inn? A: Exactly. That's where John had his office, and I was…
  • p. 320 …alone is about 24,000 miles at sea level, and about 4500 miles at 45,000…
  • p. 325 …twenty-five (25) feet at their largest sea-level diameter. The sonic unit was a combination…
  • p. 378 …per hour when one-fifth inflated at sea level). One other type of balloon which has…
  • p. 402 …Let us, then, compare the rate of leakage at any given altitude with leakage at sea…
  • p. 404 …The leakage at any altitude may be expressed as a function of leakage at sea level…
  • p. 405 Comparing rate of leakage at 40,000 feet with leakage at sea level: $$ \frac {L _ {4…
  • p. 407 …If a 20-foot diameter balloon $ \frac{1}{1 0} $ full were tested at sea level…
  • p. 408 …At sea level this is equivalent to 5.32 gm/hr. for a 20-foot diameter…
  • p. 414 …Using the rules of subsonic aerodynamics, Picard suggests that air at sea level escaping at 1333…
  • p. 415 …air at sea level (lb./ft. $ ^{3} $ ) 14.7 = pressure of air at sea level (psi…
  • p. 432 …to about 20 millibars and increased to sea-level pressure at different temperatures. The most comprehensive…
  • p. 563 …The height above mean sea level as determined from pressure measurements used in this work with…
  • p. 644 …point at which the radiosonde reaches the sea surface. ## 2. Earlier attempts There have been numerous…
  • p. 645 …The balloons floated between the surface and 30,000 ft above sea level; those which reached…
  • p. 704 …Met Gifford who has 90' sea rescue boat this project is planning to use. Stayed at…
  • p. 719 …Worzel working on gravity at sea. Saw Geo Woollard and the Ryders. Woollard after Guggenheim fellowship…
  • p. 779 …the launching site is markedly different from sea level, a shift in this curve is needed…
  • p. 817 …balloon at all times with respect to sea level. On this curve also it is customary…
  • p. 825 …The height above mean sea level as determined from pressure measurements used in this work with…
Flight 94: Released from Alamogordo, New Mexico, 1208 MST, September 3, 1948 Recovered At Villa Ahumada, Chihuahua, Mexico

On this flight, a fourth attempt was made to sustain a Seyfang, neoprene-coated nylon balloon. On Flight 79, a previous Seyfang flight, no ballast equipment had been in operation, and so a careful record of ballast flow on Flight 94 was desired. This was provided by a ballast meter. In addition to this and the barograph and Olland pressure-measuring instruments, a thermograph was also part of the equipment train.

The height-time curve (Figure 43) shows that the initial buoyancy surplus of this balloon (for the most part due to superpressure held behind

Figure 43

the safety valve) was reduced by diffusion so that after one hour of floating it began to descend at an accelerating rate. After falling about 2000 feet, the automatic ballast valve began to operate, and ballast was discharged at the rate of 20 grams per minute. During the descent, however, the strong superheat which the balloon had acquired was reduced by ventilation.

The adiabatic lapse rate of helium is $ 2^{\circ} \mathrm{C} $ per kilometer, whereas air in the troposphere warms up about $ 6^{\circ} \mathrm{C} $ with each kilometer of descent. This means that with each kilometer of fall, the lifting gas was cooled relative to the air by an additional $ 4^{\circ} \mathrm{C} $ . The combination of inertia, loss of superheat through ventilation, and adiabatic cooling of the gas as it was compressed, proved too great for the limited flow of ballast through the automatic valve, and the balloon fell unchecked to the ground.

From Flight 79, it was determined that superheat of nearly $ 4 0^{\circ} \mathrm{C} $ is built up when Seyfang balloons are flown in the sunshine. If this were lost, the buoyancy of the balloon would be reduced by one-sixth, and no satisfactory control could be achieved by ballast dropping.

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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.