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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. 228 …CBI and the Spilhaus came over later. At that time the war was going very much…
  • p. 235 …of the regular 334 that we had at sea level. From that they could deduce the…
  • p. 279 …at the Toms River Signal Laboratory, which was actually located on the jurisdictional lines between Sea…
  • p. 280 …instrument, and it was done there at the Sea Girt Inn. Q: Do you recall any…
  • p. 400 …about 24,000.m1lea at sea level, aDd about '500 allea at 45,000 feet~ Aa…
  • p. 407 …were twenty-five (25) feet at their ls.rgest sea-level diameter. The sonic unit was…
  • p. 466 …per hour when one-fifth inf~ated at sea level). One other type of balloon which…
  • 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 …of air at see level (lb./ft.3) pressure of air at sea level (psi) escape…
  • p. 520 …about 20 millibars and increased to sea-level pressure at different temperatures. The most comprehensive series…
  • 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. 736 …to identify the point at which the radiosonde reaches the sea surface. 2. Earlier attempts There…
  • p. 737 …The tensile strength at the temperatures at which the balloon flies at high altitude may be…
  • p. 801 …to <;:ee ::einnegle at office. Vet Gifford ;.;ho has 0 0' sea rescue boat this project…
  • p. 816 …Worzel working on gravity at sea. Saw Geo Woollard and the Ryders. Woollard after Guggenheim fellowship…
  • p. 887 …as the length of an uninflated bubble at the crown of the balloon. Graph 2 of…
  • p. 925 …altitude of the balloon at all times with respect to sea level. On this curve also…
  • p. 933 …Load on the gas at release (balloon plus equipment load weight). Pressure Altitude: The altitude. at…
HEADQUARTERS FITZWILLIAM FORWARD
c/o Commander, Task Group 7.2
APO 187, c/o Postmaster
San Francisco, Calif.
SONIC BALLOON TEST I KVlAJALEIN
Inclosure G to FITZWILLIAM FORWARD RepOrt
17 ll.ay 1948
The Watson laboratories of Air Materiel Command arranged for ~ne ( 1)
of its sonic balloon teams to participate in the FITZ1iilLIAM proje¢t as a
mobile team to operate in the Central Pacific, at ~AJA~IN, GUAM Qnd HICKMI.
FIElD, HAWAII, in that order, changing location for each of the thlree (.3)
explosions.
The purpose of this exploratory test was as follows: first, to deter-
mine if an atomic explosion's compressional waves are generated in the sound
channel existing between 50,000 and 701000 feet (such waves would qonce~vably
travel unirrpeded for long distances in this channel without touching the
earth's surface); second, to determine whether a sound pick-up uni~ suspended
from a floating balloon could detect compressional waves (possibly undetected
by similar sound units at the earth's surface) by virt~e of the de¢reased
background noise in the high-level sound channel.
Balloons we~e m3de of high·grade plastic, were of tear-drop a~pe, and
were twenty-five (25) feet at their ls.rgest sea-level diameter. The sonic
unit was a combination microphone-transmitter which was suspended ~rom the
balloon and picked up sound waves, transmitting them to a ground directional
antenna connected to a radiosonde receiver (standard SCR 658 air weather
radio recelver). The transmitted sound impulses were recorded on pro (2)
Esterline-Angus recorders.
;. dribble constructed of a five (5) gallon tin incorporating e 11etered
jet to allow a predetermined spillage rate of high grade kerosenerethylene-
glycol mixture was attached to the balloon. This was designed to pounteract
the helium gas seepage thru the surface -ores of the plastic ballopn. This
metered loss of ballast and controlled the rising rate of the balloon at 500
to 600 feet a minute.
Grcu.OO sonic equiJ:nent consisted ot World v:ar II sound ranging devices
utilized to pick up sound waves from an explosion traveling along the earth's
curface.
A radio receiver was used to obtain e:~tplosion time notificati1on code
signals from the ENIWETOK radio station.
The balloon launching site had to have a down-~ind clearance of about
1000 feet to lay out tho JOO feet risers and cables to which 19ere 1
attachod
the microphone-transmitter and dribbler units. Also the site had to be
sheltered from the wind to prevent da~~ge to the balloon while it was being
-1-

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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.