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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…
However, when weather conditions indicated a markedly discontinuous variation of temperature (i.e. a "front"), appropriate subjective modification of the objective linear interpolation technique was applied.

The vertical distribution of wind was determined mainly from direct observations (pilot-balloon and radio wind-sounding measurements) of free-air winds at weather stations in the area of each experiment. However, actual measurements of winds in the upper half of the troposphere often are scarce or completely lacking, and it was frequently necessary to make use of an indirect method of estimating the wind at elevations greater than 5 km. Charts of the distribution of atmospheric pressure (as given by radiosonde observations) at selected levels between 5 km and 15 km were constructed, and the wind direction and speeds at these levels were computed from the well-known geostrophic wind equation, which relates the wind to the horizontal distribution of pressure.

For the experiments carried out off the east coast of the U.S.A. between 1 August 1946 and 1 August 1947, it seemed feasible to show the distributions of both temperature and wind in vertical cross-section. This was due to the fact that these experiments were made, and the results of same recorded, within a fairly narrow band centered close to a line between Lakehurst, N. J., and Nantucket, Mass., at which points radiosonde and upper-wind observations are taken regularly. However, vertical cross-sections of temperature and wind were abandoned as a method of representation of the distribution pertaining to all subsequent experiments.

There were several reasons for this decision. In the first place, the sites and character of later experiments did not fit into the existing weather-observing network in a manner favorable to cross-sectional representation. In the second place, experience brought about the conclusion that the horizontal gradient of temperature is usually so small that, within the area encompassed by an experiment, the difference in temperature at a given level between points at the ends of a cross-section is no greater than the average error of the radiosonde measurements. Thirdly, it was soon realized that the variability of the wind in space and time is such that an individual pilot-balloon or rawinsonde ascent is not representative of the average vertical distribution of velocity during the interval occupied by a single experiment. Furthermore, as mentioned above, the wind at high levels in the troposphere often had to be inferred by indirect means. Since the true wind usually deviates somewhat from the theoretical geostrophic wind (the latter being derived under certain simplifying assumptions) and since the geometry of the pressure field is subject to some uncertainty owing to inaccuracies in the radiosonde observations, it became apparent that the assignment of a single velocity value at any

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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.