Documents / FOIA release

roswell

Office of the Secretary of Defense · 993 pages · text from the file's own layer

The Roswell Report: Fact versus Fiction in the New Mexico Desert was published in 1995 by Headquarters United States Air Force. It was written in response to Representative Steven H. Schiff's request and a General Accounting Office audit, and it contains Col. Richard L. Weaver's report and 1st Lt. James McAndrew's synopsis, along with attachments, appendices and photographs. The report says researchers found no evidence of an extraterrestrial craft or crew. It concludes that the 1947 debris came from a Project MOGUL balloon train.

  • p. 28 …In all, he estimated, the entire lot would have weighed maybe five pounds. There was no…
  • p. 231 …It was like a 500 pound rack with a receiver, frequency meter, recorder, etc., and we…
  • p. 233 …About one pound. A: correct. And the targets are nominally maybe a quarter of a pound…
  • p. 238 …They went and got a whole bunch of soo pound bombs out of the Earl Ammunition…
  • p. 258 …Third balloon with two and a half pound stick of TNT and cap set by pressure…
  • p. 263 …releasing something like maybe several hundred 500 pound bombs for this. At the same time, Trakowski…
  • p. 323 …I 4 inches wide, and weighing 13 pounds (Atch 4). The sonabuoy contained both the acoustical…
  • p. 379 …have weighed maybe five pounds. rancher living 30 mlles south. east bright wreckage made up on…
  • p. 408 …six (6) scientists and twelve (12) thousand pounds of' equipnent from BElliAR, NEV; JERSEY to KWAJALErn…
  • p. 475 …Dry ice consumption at -GOOF is approxi- mately 150 pounds for a 24-hour period. It…
  • p. 483 …is free lift in pounds and G is gross lift in pounds. Although this equation was…
  • p. 536 …New Mexico In this flight, a 65-pound load was lifted with a linear array of…
  • p. 538 …and tour larger lifting balloons, a 53-pound load was carried alott on this flight. At…
  • p. 542 …wall) to lift • total load of S5 pounds as high aa posaible (Figure 7). 'lbe small…
  • p. 588 …the AM-1 transmitter (with about 10 pounds of batteries) was received for about 400 miles…
  • p. 608 …Buoyer.cy per Pound Mol of GaS••••••••••••••••••••••••••••••••l6 V. Glossary of Term•••••••••••••••••••••••••••••••••••••••••••••21 VII. Summary of…
  • p. 614 …foot balloon should be held tinder 30 pounds; 2) ratEBot rise should be less than 900…
  • p. 621 …of 50,000 feet, with a 30-pound payload, risea about 900 feet with each kilogr…
  • p. 641 …Given: (l) The pound molar volume of any gas at standard conditions=359 ft. 3 - 15 -
  • p. 642 …2370 fte3 273.2 126 This is the mean pound molar volume at 15 km for…
  • p. 643 …foot diameter, at an altitude where the pound molar volume is 1000 ft. 3 (This is…
  • p. 715 …Suspended from the balloon is a 100 foot one thousand pound test nylon line which carries…
  • p. 736 …The solid-ballast system was complex; approxi- mately 900 pounds of sand was used on each…
  • p. 737 …It has an ultimate tensile strength of 1,900 pounds per square inch at 2SC, which…
  • p. 780 …for attaching rigging lines supporting a ~5-pound load to bottom of balloon ~nd means for…
  • p. 862 …Yii th a 20•foot General Mills balloon, using helium, a payload of 40 pounds will…
  • p. 868 …Thus, if a 40-pound load is to be lifted, it is not safe to use…
  • p. 889 …This is the volume of a pound mol of any gas at those condi- tions. By…
  • p. 893 …Elliptical shot bags, weighing 100 pounds,are used to hold the base of the bubble to…
  • p. 907 …using 15 pounds (7 kilograms) of batteries. Longer periods of transmission may be achieved by intermittent…
  • p. 984 …The detonation, or "shot" (right), of 500 pounds of TNT was monitored at White Sands Proving…
or sunset outs off the superheat is so large that it is not possible
to carry enough ballast to sustain ,the system unQ.er these condi-
tions. On the other hand, the loss of buoyancy through a sealed-off
Seyfang balloon at 4100 feet MSL is of the orQ.er of 60 grams per
hour Which is significantly less than the loss expected from a 20-
foot, 1 mil polyethylene cell in flight conditiona. (With the appendix
aperture sealed, .such a cell shows a loss of lift of about 40 grams
per hour when one-fifth inf~ated at sea level).
One other type of balloon which has been used as a super-pressure
balloon is the neoprene J2000 balloon of Dewey and Almy, surrounded
by nylon cloth shroud. The rubber balloon normally would expand
until it reached bursting diameter, but when enshrouded, it is
limited to the volume of the shroud. The difficulties in launching
and flying this balloon are not unusually great, but on each of the
several tests which have been made to date improper handling has
been a possible cause of the early rupture of the balloon. It is
believed, however, that such a balloon is not especially suitable
t~ long flights because of the deterioration which occurs in the
neoprene in the presence of sunlight. Perhaps a shroud of material
which would filter out the ultraviolet rays would protect ana
lengthen the lite of such a balloon.
Despite the success of the Japanese silk or rice-paper balloons,
which were constructed on a super-pressure principle, it is not be-
lieved practical at this time to develop a balloon of such strength
that it would successfully withstand and retain press\lre increases
corresponding to the temperature changes from night to day as the
superheat of absorbed sunlight is gained. The super-pressure with
a neoprene-coated nylon balloon, for example, would be approximaitiy
0.6 psi. That such a balloon could be built is unquestioned. The
cost of production, however, appears at this time to be unwarranted.
D. Altitude Controls
Beginning with the arrays of rubber balloons which were first used,
various systems of dropping ballast, both solid and liquid, have
been attempted with the aim of exactly compensating for the loss of
buoyancy which is occasioned as the lifting gas diffuses or leaks
through the balloon. On the early rubber balloons only rough incre-
mental ballast dropping was emPbyed. At that time it W$S decided not
to use sand as ballast since most sand contains some water which
may freeze while aloft. Further, it is easier to control the flow
of a liquid ballast than it is to control sand particles. In the
investigations for a suitable liquid ballast the petroleum product
known commercially as Mobil Aero compass fluid was finally settled
upon. These investigations included tests of cloud point, freezing
point, and also density and viscosity over a large range of tempera-
tures. The compass fluid is especially suitable for ballast work
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FOIA release, from the osd collection. The PDF is mirrored here; the original link is under it. 993 pages are in the text index: search them above, or from the library's search.