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The Roswell Report: Fact vs. Fiction in the New Mexico Desert

USAF / The Black Vault · 1995 · 882 pages · text by OCR

The Roswell Report: Fact versus Fiction in the New Mexico Desert was published by Headquarters United States Air Force in 1995. The Black Vault distributes this copy. It reproduces the report by Col. Richard L. Weaver and the synopsis by 1st Lt. James McAndrew, both written after a General Accounting Office inquiry requested by Representative Steven Schiff. The Air Force search found no evidence of an extraterrestrial craft or crew. It concluded that the Roswell debris most likely came from NYU Flight No. 4, a Project MOGUL balloon train.

  • p. 118 …Robert Gross and Mr. Maher of Lockheed 11:55 A.M. Gen. Sam Anderson 12:00…
  • p. 393 …in the form of an altitude vs. gross load chart with helium as the lifting gas…
  • p. 394 …4}{\text {Gross Load}} = \frac {K}{W} $$ In turn, $ \frac{K}{W}=a e^{-0. 4…
  • p. 395 …free lift in pounds and G is gross lift in pounds. Although this equation was derived…
  • p. 400 …By equation (10), with a gross load of 52 kg., the unbalance caused by loss of…
  • p. 412 …or a gross buoyancy of 450 lb., the maximum allowable inflation of a 30' diameter, .001…
  • p. 479 …accelerating force equal to 5% of the gross load (52 kg) was acting to bring the…
  • p. 552 …000 feet. In one step, this becomes: Gross Lift/Balloon = (Balloon Volume) x (Difference in molecular…
  • p. 555 …of rise in feet per minute G = gross lift in grams For our purposes, we wish…
  • p. 559 …G) ^ {\frac {2}{3}} $$ (Approximate) where G = gross load A chart, Figure 24, has beendrawn up…
  • p. 561 …where $ \triangle G= $ loss of lift G = gross load (balloon weight plus equipment load) $ \triangle T…
  • p. 562 …not including balloon or its integral parts. Gross load: Load on the gas at release (Balloon…
  • p. 635 …Serial No. ___ description ___ ___ Line length ___ Banner description ___ ___ Ballast assembly - description ___ ___ Eallast. ___ Total Equipment Weight. ___ Gross Load ___
  • p. 636 …Gross Load . . . ___ Assumed Gross Lift (Gross Load + 10%) G ___ G 2/3 ___ Free Lift - F = $ (\frac…
  • p. 649 …theoretical altitude determined by the displacement and gross load. ## 7. Control systems Two systems of control…
  • p. 681 …By adjusting the gross load to be supported by the gas to equal the total lift…
  • p. 691 …A chart showing the relation between altitude, gross lift, and balloon size has been found necessary…
  • p. 775 …The gross load reported should be accurate to the nearest 200 grams. The amount of lifting…
  • p. 777 500 gm DRAG CHUTES 300 " BANNER 2000 " PAYLOAD 4500 " BALLOON 7300 " GROSS LOAD ## NOTE: Use low…
  • p. 779 …bubble length and resultant inflated volume, using gross lift as an expression of volume. It will…
  • p. 781 …in Appendix II summarizes the relationship between gross load and floating level for balloons of several…
  • p. 817 …A can of sand is made to weigh the same amount as the required gross lift…
  • p. 825 …the balloon with the equipment load attached. Gross Lift: Lift of all of the gas in…
  • p. 830 …Serial No. ___ description ___ Drag chute ___ ___ Banner description ___ ___ Ballast assembly - description ___ ___ Ballast ___ Total Equipment Weight . ___ Gross Load . . . . . . . . . . . . . . . . ___
  • p. 831 …waiting___ grams Actual balloon lift . . . . . . . . . . . ___ " AActual gross lift (Balloon lift & balloon wt.) . . . . . ___ " Number Helium tanks required…
  • p. 835 …Gross Lift vs. Bubble Length . . . . . . . 107 Graph 3: Buoyancy vs. Altitude . . . . . . . . . . 108 Graph 4: Gross Load…
  • p. 847 …Estimated Gross Load Limit kg. Altitude Range ft. 7 200 0.6 1.5 to 5…
received satisfactory results when the number of targets was increased to between 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 employed on flight nos. 3 and 4, but it was only marginally successful. This prompted Moore and his associates to configure the two remaining flights of Alamogordo I, flights #5 and #6, with radiosonde transmitters.

For these two final flights, Moore devised a method of manually determining azimuth and elevation, in the absence of a radisonde recorder, by counting clicks as pressure-sensitive contacts closed. NYU Technical Report No. 1 shows two "interpretations" of the data which confirm that manual calculations were used. In regard to flight no. 5, it appears there was a typographical error in Technical 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 diary (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. 1-6 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 No.1, Table VII	Sandy Hook, NJ
2	4/18/47	Bethlehem, PA	See Appendix NYU Special Report No.1	Unknown
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 No.1, Table VII	East of Roswell, NM
6	6/7/47	Alamogordo, NM	See NYU Tech. Report No.1, Table VII	South of Highrolls, NM

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Report, cited by the archive. The PDF is mirrored here; the original link is under it. The text was read from the page images by an OCR model; expect the odd misread word. 882 pages are in the text index: search them above, or from the library's search.