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.

  • 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…
Since the back pressure forcing the helium out of a
full balloon When it is rising is 4 times as great at
1000 feet per minute as at 500 teet per minute, the rate
of rise is critical when an appendix is used. It has
been found necessary to limit the rate of rise to 700
feet per minute to prevent bursting at ceiling when using
General Mills 20-foot balloons with standard appendix.
It is believed, from laboratory tests, that use of the
spring bow stiffeners on the new appendix will permit rates
of rise up to 1000 feet per minute. Flutter in the bal-
loon fabric while rising is apt to cause failure due to
ripping at speeds of more than 1000 feet per minute. A
20-foot General Mills balloon will burst with an internal
pressure of 0.014 psi., which is about 1mb., equivalent
to a 200-foot rise at ceiling with a closed appendix.
III. EQUIPMENT TRAIN
A. Lines and Rigging
Following rigging failures early in the testing program,
careful study was given to the lines and rigging methods
used to attach flight instruments to the balloon. For
safety in launching, a factor of 10 to 1 is used on all
loads. Thus, if a 40-pound load is to be lifted, it is
not safe to use less than a 400-pound tested line. The
line strength should be determined independently if
possible, since the actual breaking point of lines runs
between 50 and 70'/o of the manufacturer's rated strength.
Braided or woven nylon is recommended for all rigging.
A stranded or laid line is subject to untwisting in flight,
twirling the suspended instruments and reducing line
strength. The nylon material is weather resistant to a
high degree and tends to stretch under shock rather than to
snap. For some purposes it may be desirable to use a line
of constant length, in which case the nylon may be pre-
stretched. Only a few of the common knots are useful
in tying nylon. Bowlines and square knots have been found
to slip and are hard to untie. The carrick bend, shown
in Figure ~is recommended. ln addition to this, a safety
knot is made in the loose end, and the entire tie secured
by a final taping. For convenience in assembly, the indiv~
dual pieces of line and equipment are rigged with harness
snaps at each end. This permits unit replacements or re-
moval at the last minute with a:t minimum of delay. For
extremely light-weight rigging, wooden toggles and loops
in the nylon may be used instead of the heavier metal
snaps.
-14-

Cases discussed

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.