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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…
The actual atmospheric distribution. however. does not indicate an
adiabatic lapse rate for air but rather a lapse rate which varies
with altitude. For. the troposphere the lapse rate of the atmosphere
averages -1.980C/1000 .ft. It may be shcrrm then that in the tropo-
sphere a rising balloon will get warm with respect to the air
(neglecting ventilation and radiation effects} at a rate of
1.98 - .57 : 1.4lOC/lOOO ft. In the tropopause the lapse rate of
the atmosphere is zero. Thus the lifting gas (if helium} will
oool relative to the air at a rate of .570C/1000 ft.
Similarly, in the stratosphere, the lifting gas will cool relative
to the air at a rate of 2.24 ~ .57 : 2.81°0/1000 ft. This effect
is plotted as Figure 22.
...0
:;)
TEMP. OF LIFTING
GAS DUE TO
AD.IABATIC EXPAN-
SION WITH AL'riTUDE
STRATOSPHERE
~ TROPOSPHERE
~~----------------\---~--~~~~~~~
c
TEMPERATURE
Figure 22. Lapse rate of air and helium.
Here. below point A, the lifting gas will be warmer than the air.
Above point A, the lifting gas will be cooler than 'the e.ir. The
effect of this temperature difference on the lift (as shovom in the
previous section} is approximately lll = L ..ai I
T (I- 8)
Thus. as a balloon system passes through point A. it will have less
lift then at release. This effect has been observed on several
flights. where a balloon system slowed down during ascent through
a ~mperature inversion.
Since the effect of the sun in heating the lifting gas decreases
the effect of different lapse rates, the effect is not as noticeable
during the day as at night. At night the balloon system may pass
through an inversion, lose its lift, and remain at an altitude much
below its estimated floating altitude until warmed by the sun's rays
at sunrise.
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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.