Documents / FOIA release
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.
“Sea”26 pages
- 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…
the same time that ballast is normally required in flight. T.his
system simulates the effect of rising and falling in the atmosphere
and indicates the effectiveness of the controls which have been app~d.
In order to simulate flight, it is necessary that three conditions
be mainta·ined within the system. The first is that a leak of air
into the bell jar is pennitted at a rate of pressure increase which
has been observed during balloon descent. A large lag chamber is
connected into the bell jar to supply the second condition which
is a delay similar to that inherent in the control action on an actual
balloon flight. It is •necessary to properly adjust the vo!ume of
such a lag chamber to obtain the desired magnitude of control action.
A third requirement is that the response of the vacuum pump must
correspond to that response which has been observed when a balloon
system drops ballast. In order to measure this, the control me-
chanism has been allowed not only to switch the vacuum pump on and
off but also to actuate the standard ballast-flow equipment. This
system may be adjusted so that the amount of pressure change which
a single period of pumping produces accurately represents the amount
of ballast thrown off during flight.
T.he barogram shown in Figure 18 is e.n example of such a test. On
this test the re.te-of-ascent ballast switch v.ras added to the displace-
•Hours •
Fhaht Samahtude Record Of Pressure
A- Oasplacement Swatch
OperatanQ.
B- Oaspl. a Rate Of Ascent-
Swatches OperahnQ.
Figure 18. Sample barograph record.
ment switch after the latter had operated for a period of six hours.
The combination of the two is seen to have effected a reduction in
-26-
About this file
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.