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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…
When the total quantity of gas needed has been computed,
the lift requirement may be expressed in terms of the
pressure of a number of cylinders of gas. It is not
possible to assume that each tank of gas will give the
same amount of lift, nor is it possible to use a gage
which has not been expertmentally calibrated to relate
lift to pressure. For calibration of a gage it is suffi-
cient 'eb valve gas from an observed equilibrium tempera-
ture and pressure in a cylinder into a rubber balloon
8:ll4 then measure the total lifting capacity o! the gas
from the tank. Check points should be made with tanks
under varying amounts of preseure. Figure 19 shows a
sample gage oalibration worked up for varying temperatures
auUJiling the simple gas law
Lift2 : ..£2._){....!1_ Lift1
pl 1'2
This law applies to w1 thin !1%. Note: Do not use Graph 6
without checking calibration of gage to be used. Ordi-
narily a whole number of full tanks of gas will not
exactly supply the desired lift,which should be figured
with not more than one-tenth tull tank tolerance in ex-
cess (penni t no under inflation). It is thus necessary
to prepare partially full tanks and by combining full and
partially full cylinders get the required total. It is
necessary to allow the cylinders to attain equilibrium
temperature after valving them before taking final pressure
readings.
B. Length of Balloon Bubble
The volume of gas required for a given balloon may be ex-
pressed as the length of an uninflated bubble at the crown
of the balloon. Graph 2 of Appendix II gives the relation-
ship between bubble length and resultant inflated volume,
using gross lift as an expression of volume. It will be
noted that when the elevation of the launching site is
markedly different from sea level, a shift in this curve
is needed to accomodate varying densities of the atmosphere.
The inflation of this bubble, which is pinched off by
launching equipment or shot bags, will serve as a good
check of the final amount of gas in the balloon, thus
warning if the balloon is underinf'la ted.
c. Expected Altitude
To predict the altitude to which a balloon will rise it
is necessary to know the volume of the balloon, the total
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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.