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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…
received satisfactory results when the number of targets was increased to belo/een
3 and 5.30 Interestingly, during July of 1948, a similar test would be made at
Alamogordo AAF by another organization.31 This test confirmed Moore's theory
that when targets were increased to at least three, satisfactory returns were
received by the radar. This procedure, according to Moore, was employe~ on
flight nos. 3 and 4, but it was only marginally successful. This prompted Mioore
and his associates to configure the two remaining flights of Alamogordo I, flights
#5 and #6, with radiosonde transmitters.
I
For these two final flights, Moore devised a method of manually determi!ning
azimuth and elevation, in the absence of a radisonde recorder, by counting dicks
as pressure-sensitive contacts closed. NYU Technical Report No. 1 shows 1
two
"interpretations" of the data which confirm that manual calculations were q.sed.
In regard to flight no. 5, it appears there was a typographical error in Techpical
Report No. 1, Table VII, for the time of launch which is erroneously listed as 1517
MST, contrary to figures 32 and 33 in Technical Report No.1 and Crary's qiary
(Atch 6). The correct time of launch for flight no. 5 appears to be 0516 MST. With
the launching of flight no. 6 at approximately 0530 on June 7, the NYU group
departed Alamogordo via a B-17 for Newark AAF, NJ. NYU flight nos. 1~ are
summarized below:
SUMMARY OF FLIGHTS 1--6
Flight no. Date Launch Site Configuration Landing: Site
1 4/3/47 Bethlehem, PA See NYU Tech. Report Sandy Hoof<, NJ
No. 1, Table VII
2 4/18/47 Bethlehem, PA See Appendix NYU Unknown
Special Report No. 1
3 5/29/47 Alamogordo, NM Same as flight no. 2* Unknown
4 6/4/47 Alamogordo, NM Same as flight no. 2* Unknown
5 6/5/47 Alamogordo, NM See NYU Tech. Report East of Roswell, NM
No. 1, Table VII
6 6/7/47 Alamogordo, NM See NYU Tech. Report South of H'ghrolls, NM
No. 1, Table VII
* Depictions of flight nos. 3 and 4 are not provided in the NYU reports. According to NYU Progress ~eport
No. 6, Section II, p. 5, the equipment to be used for the Alamogordo field trip in June was consistent with
the depiction of flight no. -2. This information also concurred with Crary's partial description of flight no. 4
in his diary. ·
Note: An attempt to launch a balloon-train assembly which would have been NYU flight no. 3 was made
on May 8, 1947, but due to strong winds, restraining lines failed before the acoustical payload was attached.
Since the launch was unsuccessful, no flight number was assigned.
30. Ibid.
31. Rprt, Holloman AFB, "Progress Summary Report on U.S.A.F. Guided Missile' Test
Activities," Vol 1, Aug 1, 1948.

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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.