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…
which switches four elements into the transmitter circuit in turn.
Recently a motor making five revolutions per minute was used so
that each temperature is transmitted for three seconds. The four
elements are the free-air temperature, the gas temperature, battery-
pack tempereture and a reference signal. This switch is supple-
mented by a master program switch whicp alternately places the
temperature switch and the pressure modulator into the transmitter
circuit. The present arrangement is to permit the temperature data
to be transmitted for about one minute in every fifteen. In this
wt.y represente.tive temperature sampling may be obtained, without
materially destroying the continuit,y of the pressure and ballast
data.
A second system or determining temperature makes use of the smoked
drum of the barograph. By adding a temperature-activated pen, this
unit makes a record of the temperature encountered. Since it is not
the free-air temperature nor the temperature or the lifting gas but
rather the temperature or the barograph itself, the data obtained
has been or little value. Following the development of suitable
temperature telemetering apparatus, this method was not used.
c. Ballast Metering
It is often very desirable to knowwl'ether or not ballast control
equipment is operating properly during flight tests. For this
purpose, two ~stems of ballast metering have been devised. It is
possible (1) to record on an instrument which is balloon-borne or
(2) to detect and telemeter information to the ground concerning
ballast flow.
Figure ~7 shows the automatic siphon which has been used in the AM-1
transmitter circuit for the telemetering of such information. A
series of pulses of fixed frequency is transmitted whenever the
contact arm of the automatic siphon is filled above a critical
level. The electrolyte used is non-miscible with the ballast and
rises and falls in proportion to the rise and fall of the aain arm
of the siphon. This main arm empties when approxiDIIltely 3.5 grams
ot ballast have been allowed to flow into it. As a consequence of
this intermitte~t filling and emptying of the lines of the siphon,
an intermittent slgnal of f'ixed.frequency is transmitted whenever
ballast is flawing steadily. It is important that an electrolyte
be used wHich will not freeze at low atmospheric temperatures and
will not boil at the low pressures encountered. After a aeries of
tests it was decided that a G4% solution of hydrochloric acid be
used for altitudes up to 85,000 teet. It is necessary to use
platinum wire for the contact points.
In order to record in flight the functioning or the ballast control
system a ballast recording mechanism has been developed in con-
junction with the Lange Laboratories of Lexington, Kentucky. This
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About this file

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.