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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…
mass-production methods and quality control associated with standard dry batteries gave greater assurance of satisfactory performance.

Subsequent measurements made of the temperature inside the transmitter battery pack showed that the temperature can be maintained above -10 $ ^{\circ} \mathrm{C} $ if the transmitter and batteries are housed in a box insulated with one- to two-inch walls of Styrcfoam. This insulation is effective even through long nighttime periods when no solar heating is added.

One type of battery tested in flight was a light-weight wet cell (Burgess Type AM) of the "dunk" type, (magnesium + silver chloride). These cells were vacuum-packed to provide indefinite shelf-life. Activated by immersion in water just before release, they were expected to produce a constant voltage over a period of 6 hours to overcome cold temperature effects. Those units used proved to be rather unsatisfactory and subject to erratic behavior. Furthermore the cost of the cells was very great compared with ordinary cells.

## E. Radio Direction-Finding

For ground stations, when the balloon-borne transmitter is a T-69, the SCR-658 RDF set has been used. With such a set the radio signal can be picked up at distances up to 150 miles and good azimuth bearing may be obtained (accurate to less than one degree). Although the elevation angle may be obtained with equal accuracy when free from distortion, angles of less than 13 degrees are usually affected by ground reflection to such an extent as to render them valueless.

To extend the range over which such sets were effective, two or more usually were used, positioned along the expected track of the balloon at intervals of about 100 miles. With two sets giving crossed azimuth "fixes" the position may be determined. If the elevation angle is above 13 degrees, it is possible to fix the balloon with one SCR-658 (assuming the pressure altitude is known).

For details of the maintenance and use of the SCR-658, see War Department publication T.M. 11-1158A.

When aircraft are used to follow and position the balloon, the use of a radio-compass is found to be feasible, using the AM-1 transmitter at a frequency that is within the limits of the compass receiver. By homing on the signal and flying along the indicated bearing until the compass needle reverses, the balloon's position may be found from initial distances of up to 500 miles. No appreciable cone of silence has been observed in recent flights which used a transmitter operating at 1746 kc.

Radio compass equipment, AN/ARN-7, is described in U. S. A. A. F. publication T. 0. 68-10.

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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.