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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. 36 …potential existence of such records within DOE channels, however. An Extraterrestrial Craft The Air Force research…
  • p. 81 …is not normally released outside Air Force channels. It does not cover the investigation of air…
  • p. 214 …Some of the reflectors were procured from sources out of normal channels. Some of the contractors…
  • p. 236 …try to put microphones into the sound channel. During WWII, the ·signal Corps had laid on…
  • p. 240 …I knew, just being an atmospheric physicist, I knew about the sound duct channel and I…
  • p. 273 …the sound waves operating in the sound channel in the stratosphere. The constant level balloon was…
  • p. 279 COL TRAKOWSKI - 6/29/94 7 were out of channel, so to speak. It was on…
  • p. 319 …II, studying, among other things, the "sound channel" in the ocean. He proved that explosions could…
  • p. 399 …Tb1e situation 1s~escr1beo a• a sound channel .. 1tb 1t& axis at 4000 feet, because all…
  • p. 400 …that there is a s1~1lar sound channel 1n the atmosphere with the axis at a…
  • p. 401 …red height withqut prohibit1'Ye eacr1t1ce ot sound channel prooertiea. Hawcner, 1~ the aub:a.rine…
  • p. 402 …cted at tbe axis ot the sound channel ahould be made. In·., op1n1oii', the J)r1nc1…
  • p. 403 …toe ~trato::.;;he:r·a so\,;nd channel ~!:lould be 1r.ves:.:1. 0ated, for it…
  • p. 407 …compressional waves are generated in the sound channel existing between 50,000 and 701000 feet (such…
  • p. 432 …ratio) and simultaneous transmission of several data channels at one frequency. This project was abandoned before…
  • p. 434 …The recorder used was a Brush BL-202 dottble channel oscillograph. A. quarter wave vertical receiVing…
  • p. 525 …To permit the transmission of both temperature and pressure data by one radio channel, a pe…
  • p. 671 …her than pressure is also to be transmitted on the same radio channel, the pressure - 33 -
  • p. 802 …Discussed with Crane possibilities of getting sound through the ground part of the ocean sound channel…
  • p. 980 …It was Ewing who first conceptualized the military significance of the atmospheric sound channel. His proposal…
Flight 12 was designed to overcame the difficulties encountered
in flights 8 and 11, and, by the use of a thin tear-drop balloon (General
Mills balloon) to earn~ the load to a higher altitude than flight 10.
To guarantee a predetermined constant ballast flaw, the manual ballast
valve we.s added to the flight train. The minimum pressure switch
replaced the fixed pressure switch to activate the automatic ballast
valve, whether or not a predete~ined activation altitude was reached.
Figure 46 shows the train; figure 47 shows the time-altitude curve, Which
exhibits a marked departure from the ideal. The minimum pressure switch
failed to operate or operated near surface pressure, effectively preventing
the operation of the automatic ballast valve. The manual ballast valve did
not provide sufficient rlow to prevent the gradual descent of the balloon.
Finally, the heavy load necessitated almost complete inflation of the
balloon at the surface. lhis distention permitted continual mixing of
air through the open bottom of the balloon. Instead of reaching the pre-
calculated 38,000 feet maximum altitude, this flight had a peak of 14,000
feet from which it slowly descended. Since the blowout patch was set to
act upor. descent to 20,000 feet, it also failed to operate.
Five of the succeeding flights (nos. 13, 14, 15, 16 and 20) had as
a prime objective the development of a satisfactory a.ppendix to overcome
the loss of buoyancy due to mixing during launching and ascent. fhe types
considered have been discussed in Section II, Part A of this· report and
the (two foot) appendix stiffened with battens, Which was finally evolved,
is shown in figure 5. Figures 48, 49 and 50 show the time-altitude curves
for these flights. Either short flight or limited radio reception curtailed
the trajectory data.
In flight 19, the danger to perscrmel of the blowout patch was
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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.