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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…
Retention: Indefinite. No known replacement in the AAF.

Duties: Chief, Electronic Plans Section, Electronic Subdivision. This officer should be retained in his present assignment due to the background of knowledge and experience which he has with reference to electronic research and development as well as meteorological research and development and the physics of the upper air. Colonel Maier has completed all requirements for a Ph. D. degree from the California Institute of Technology except for six months residency. During the period 1 February 1945 to 1 January 1946, Colonel Maier had been Commanding Officer of Watson Laboratories in charge of research and development of ground radar, radio and electronics equipment peculiar to the Army Air Forces, previous to which he was in command of various Signal Corps laboratories. Furthermore, he has complete technical knowledge and understanding of the projects being carried on by Watson Laboratories and Cambridge Field Station, which can only be achieved by years of active participation in the actual research and development of that particular type of electronic ground equipment.

Colonel Marcellus G. Duffy. 0-18373

Retention: Indefinite. No known replacement in the AAF.

Duties: Assitant Chief, Electronic Plans Section, Electronic Subdivision. This officer has an extensive background and knowledge in meteorological and electronic research and development. He is a graduate of M.I.T. in meteorology. Colonel Duffy was liaison officer from the Commanding General, AAF, to the Chief Signal Officer for duty in connection with meteorological equipment for the period 1942-1946. During this period he set up AAF requirements, standards and training programs for weather equipment and personally followed this equipment from the laboratories to its introduction in all combat theaters. From September 1946 to January 1947, Colonel Duffy was in charge of applied propagation of compressional and magnetic waves at Watson Laboratories. At the present time, Colonel Duffy is monitoring the upper air research program for the AAF in addition to his duties as Assistant Chief of the Electronic Plans Section. With the Air Force competing against other services in the upper air research program, guided missiles and meteorological research, a competent, practical and theoretical officer is considered essential in the Plans Section, Electronic Subdivision.

Colonel Ralph L. Wassell, O-22329

Retention: Indefinite. No known replacement in the AAF.

Duties: Chief of Operations for Power Plant Laboratory. In this capacity he is responsible directly to the Laboratory Chief for the planning and execution of the entire engine development program. Specifically, he is responsible for supervision of the Rotating Engine Branch and the Non-Rotating Engine Branch. In order to successfully execute his responsibilities, Colonel Wassell must coordinate and approve the initiation of all research and development projects for

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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.