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. 129 …6099 2 HQ AMC WRIGHT PAT 342-seA-6191 CAMBRIDGE LABS 342-A~ AMC HQ WRIGHT…
  • p. 228 …overhead and followed the balloons out to sea. I have no idea about the results that…
  • p. 235 …the regular 334 that we had at sea level. From that they could deduce the temperature…
  • p. 279 …actually located on the jurisdictional lines between Sea Girt and Springlake, New Jersey. It was an…
  • p. 280 …The Sea Girt Inn? A: Exactly. That's where John had his office, and I was…
  • p. 400 …alone 1a about 24,000.m1lea at sea level, aDd about '500 allea at 45,000…
  • p. 407 …five (25) feet at their ls.rgest sea-level diameter. The sonic unit was a combination…
  • p. 466 …hour when one-fifth inf~ated at sea level). One other type of balloon which has…
  • p. 490 …Let us, then, compare the rate of leakage at any given altitude with leakage at sea…
  • p. 492 …The leakage at any altitude may be expressed as a function of leakage at sea level…
  • p. 493 Comparing rete of leakage at 40,000 feet with leakage at sea level: ~ 188 .u§. - 0…
  • p. 495 …It a 20-foot diameter balloon~ full were tested at 10 sea level and found to…
  • p. 496 …At sea level this is equivalent to 5.32 ~r. for a 20-foot diameter balloon…
  • p. 502 …Using the rules of subsonic aerodynamics, Picard suggests that air at sea level escaping at 1333…
  • p. 503 …sea level (psi) escape velocity of air to produce back pressure of 1 atmosphere at sea…
  • p. 520 …to about 20 millibars and increased to sea-level pressure at different temperatures. The most comprehensive…
  • p. 654 …The height above mean sea level as determined fram pressure measurements used in this work with…
  • p. 686 …to a thtmble a.nd attached to re1n forced pCltches at alterna.te .sea.m.s…
  • p. 688 …lQr9e Ba.lloo n ~hould trQin de .sea nd to 101000'. 6 each.-Gene ral M1lls…
  • p. 736 …point at which the radiosonde reaches the sea surface. 2. Earlier attempts There have been numerous…
  • p. 737 …The balloons floated between the surface and 30,000 ft above sea level; those which reached…
  • p. 801 …Vet Gifford ;.;ho has 0 0' sea rescue boat this project is planning to use. Stayed…
  • p. 816 …Worzel working on gravity at sea. Saw Geo Woollard and the Ryders. Woollard after Guggenheim fellowship…
  • p. 887 …the launching site is markedly different from sea level, a shift in this curve is needed…
  • p. 925 …balloon at all times with respect to sea level. On this curve also it is customary…
  • p. 933 …The height above ~ean sea level as determined from pressure measurements used in this work with…
difficult, but if the two elliptic.al shot bags are em-
ployed, they must be lifted simultaneously upward and
outward away from the balloon. As the cell rises, each
piece of gear must be cradled by its bearer allowing it
to be lifted vertically when the balloon passes overhead.
In many instances where the wind direction is ~ot constant
at the surface or changes as the balloon goes upward, and
exact downwind positioning of launching personnel will be
difficult. It is often necessary for these men to run to
one side or forward or baekward to get directly beneath
the balloon. In cases of extreme wind speed, it has been
found necessary to load the lower pieces of equipment on to
a truck bed before release of balloon and launch 1t by
driving underneath the balloon.
It is possible to estimate the space required to launch a
train of given length if the wind speed is known. By using
the computed figure for rate of rise, the length of time re-
quired to lift the entire train is found. The distance
the bubble will travel during this time is proportionate to
the wind speed. For example, if a train 250 feet long is
launched with the rate of rise at 500 feet per minute, a
bubble will move downwind at 660 feet if the wind is 15
miles per hour (22 feet per second), and the man at the end
of the equipment train must cover 410 feet in 30 seconds
carrying the gear with him.
The use of a restraining line attached to the load line above
any heavy gear or delicate gear is recommended. A loop in
this restraining line is attached to a winch mounted on a
track a few hundred feet downwind of the lowest piece of
gear, or is held by a well-gloved man. The safety ~~ights
are attached near the end of this line. The balloon tends
to pull the gear in beneath itself in calm or light winds,
and may pull sidewise if the train alignment is not perfectly
downwind; the restraining line withstands this pull. Thus
tethered, the b•lloon is forced to come overhead of the equip-
ment bearers, and they are able to launch with less diffi-
culty and danger of equipment damage. If the apparent ascent
rate is too slow, the restraining line is cut between the
.safety weights and the other pieces of equipment. If the rate
of rise appears to be high enough, the restraining line is
severed below the safety weights and they rise, completing
the launch:i.ng.
VII. TRACKING AND ALTITUDE DETERMINATION
Following release, it is often necessary to know the position
of the balloon and its height as long as possible. Several
methods of position and height determination have been found
useful. Advantages and limitations of each system are given.
-51-

Cases discussed

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.