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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. 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…
F. Flight Termination Gear
The rate of descent when controlled balloons are falling after
exhausting all ballast is sometimes as slow as 50 feet per minute.
This means that several hours might be required to fall through
the lanes of aircraft traffic, increasing considerably the hazard
to aircra.ft (admittedly very small). To minimize this possibility,
units have been added to the flight train to cause a rapid descent
after the balloon system has descended to some critical value, say
20,000 feet. One such destruction system, using a flight-termination
switch, is shown in Figure 21. It consists of a pressure-activated
switch, triggered on descent only, an explosive charge used to sever
KNOT&. Aaovs
A ioa D Snow CAN >lOotS
34' RP UIIE__...
OF 100* TEST
BRAIDEO NYLON
WaTH 2' SLACK
O&TAIL OF R•P L.I'NS
.... , .. 'T iMTb BAI.LOON
~
~ ld.ueLINECcouD •) 10 1lUE.
PI.AGE fW IfT .......ItCH IN
BEEN CUT ( IIOIJIIO Willi TIKAD)
"'-fi..aaHT"iRMMeAroaS..lttiRR
BALLOON ON FINAL DESCENT 10
2(\000 tT1 1Ml15I4EiltJC.IM(:,
I'Ulo\TlM& liME .. ntEAIR LANES,
lME HALF DI::F\.,t,l~D ~LCCllt lltD
ACTS A5 1rs CJWN PAR~C ...ITE
Figure 21.. Flight termination equipment.
the main load line, a rip line attached to ·the balloon near the
equator anQ. a snub line which takes up the strain after the load
has fallen a few feet.
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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.