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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…
decreasing the coefficient of coupling between the primary and secondary of the IF transformers. By this reduction of bandwidth to 3kc a 3 microvolt signal produced a 15.5 DB signal to noise ratio, where at 16 kc bandwidth only 7 DB was obtained.

In order to obtain accurate reproduction of the amplitude of the audio frequency the AVC circuit was modified by adding a fixed bias to the AVC diode of the receiver. This flattened the characteristic of the AVC circuit and no change in amplitude of recorded audio signal was detected over a six hour flight using a constant amplitude audio signal from the transmitter. The signal was tapped off at the output of the second detector of the receiver and fed to a Brush BL 905 AC amplifier for recording. The recorder used was a Brush BL-202 double channel oscillograph. A quarter wave vertical receiving antennae was employed with a counter poise ground. The transmitting antennae was a vertical half wave dipole.

In order to use the AM-1 for transmission of information from pressure and temperature sensors a relaxation oscillator circuit was incorporated in the system. (dotted section - Fig. 6). This oscillator used one half of one of the 3A5 modulator tubes and produced a blocking rate approximately proportional to resistance of the sensor instruments. This information could be superimposed on the regular modulated signal and two types of information could be transmitted simultaneously; one as amplitude and frequency change of the basic signal, the other as a frequency of pulses superimposed on the basic signal.

The AM-1 has been used in balloon control research to transmit information on pressure, temperature and ballast requirements. It was also employed to give information on Neutron intensities in another Air Force project(5). In order to obtain information on balloon position on a wind study project the AM-1 was used as a beacon to be "homed in" on by the radio compass of aircraft(6).

A system of diversity reception was considered for use with a dual channel AM-1 transmitter in order to increase reliability despite atmospheric noise. In the dual channel unit a common modulator was connected to two separate crystal oscillators and RF amplifiers. In preliminary tests two receiver and recording units were used.

For short range balloon flights the AM-1 was modified for use with subminiature and acorn type tubes. In this, the AM-2, two 2E27 tubes in parallel provide excitation for the type 958A RF amplifier. A circuit diagram of this unit is shown as Fig. 7.

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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.