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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. 143 …Robert Gross ar.d 't!r. Jlaher of Lockheed 11~ 55 A.'.!. Gen. Sam Anderson 12…
  • p. 481 …Balloon Volume x Gas Lift Gross Load · It may be noted from this equation that a…
  • p. 482 …Balloon Volume x 24.4 Gross Load K =-w K _ 08.o475Z In turn, w-in…
  • p. 483 …free lift in pounds and G is gross lift in pounds. Although this equation was derived…
  • p. 488 …By equation {10), with a gross load of 52 kg., the unbalance caused by loss of…
  • p. 500 …or a gross buoyancy of 450 lb. • the maximum allowable infle.tion of a 30' diameter…
  • p. 569 …accelerating force equal to 5% of the gross load (52 kg) was acting to bring the…
  • p. 643 …000 feet. In one step, this becomes: Gross Lift/Balloon = (Balloon Volume) x (Difference in molecular…
  • p. 650 (Approximate) where G • gross load A chart, Figure 24, has beendrawn up, based on this equation…
  • p. 652 …G = loss of lift G =gross load (balloon weight plus equipment load) AT : mean temperature difference…
  • p. 653 …not including balloon or its integral parts. Gross load: Load on the gas at release (Balloon…
  • p. 726 …Ballast • • .. • • '" • Total Equipment l~eight. • • • • ' Gross Load • • ' • • • • {56)
  • p. 727 …Balloon volwne x gas litt/mol gross load cu. ft. -----------------NAximum Altitude • • • ft, m.s.l…
  • p. 741 …altitude deter- mined by the displacement and gross load. 7. Control systems Two systems of control…
  • p. 777 …By adjusting th~ gross load to be supported by the gas to equal the total lift…
  • p. 787 …Computations A chart showi~ the relation between altitude, gross lift, and balloon size has been found…
  • p. 883 …The gross load reported should be accurate to the nearest 200 grams. The amount of lifting…
  • p. 885 …A L L 0 0 N 7300 ,, GRoss LoAD Fl G. 17 NYU BALLOON pROJECT I…
  • p. 887 …bubble length and resultant inflated volume, using gross lift as an expression of volume. It will…
  • p. 889 …in Appendix II summarizes the relationship between gross load and floating level for balloons of several…
  • p. 925 …A can of sand is made to weigh the same amount as the required gross lift…
  • p. 933 …the balloon with the equipment load attached. Gross Lift: Lift of all of the gas in…
  • p. 938 …description.______________ Drag chute ---------------------------- Banner description --------------- ---------- Ballast assembly - description -----------~-- Ballast • • • • • • Total Equipment i'ieight • • ' • • • • • • Gross Load • • • • • • • • • • • -86-
  • p. 939 …wnitin_,g________ grams Actual balloon lift • • • • • • • • ". . .• II AActunl gross lift (Balloon lift & balloon wt.) • Number Helium…
  • p. 943 …Gross Lift vs. Bubble Length • • • • • • .107 Graph 3: Buoyancy vs. Altitude • • • • • • • • • .108 Graph 4: Gross Load…
  • p. 955 …BALLOOO DA 'fA General Mills Actual Balloon Estimated Gross Altitude ~ominal Diiameter Volwne Weight Load Limit…
A review of this systEm by members of the University staff
has b4}ell published in "Transactions of the American Geophysical
Union{2}11 Earlier work on this development has been reported
by members of this Research Division in"Technical Report 93·(or(3)
and in the "Jo11rnal of the American Meteorological Society" 4).
A manual for those interested in making use of balloon syste.s
of this type has also been published as "Section II, Operations"
of our "l'eclmical Report 93.02 11 (1). This report consists of a
disc,1ssion o.f instrumentation for balloon systems, techniques
for launching and tradtng, and telemetering from balloons as
developed and tested at New York University.
c. Telemetering From Balloon Systems
The second requirement of this project was the_investigation,
development, and testing of balloon borne telemetering systems. ( )
The development was completed in June of 1948 and a final report 7
of work accomplisred and recommendations made to the sponsor at
that time.
Two types of transmitter ,nits were suggested as a means of
accomplishing ~he telemetering of data from a balloon to ground
station receivers. A high freq,1ency syatea, making use of line-or-
sight transmission allows for accurate positioning of the balloon
system from two' ground stat~.ons. The line-of-sight characteristic,
however, limits the range of this type transmitter, and ranges
in excess of 250 miles are not to be expected with a balloon
system floating at 40,000 ft.
Three line of sight transmitters were designed for use in
balloon work. The first, the FM-1, was designed to operate at
72 me, using a conventional reactance tube modulator. Several
stages were included to deliver 1 watt o~tput at tbe design
frequency. The unit was cruitP. complicated and the required
input :oower large due to the requirement for several stages
to transmit at the high frequency. Fig. 4 is a schematic of
the FM-1 transmitter.
In order to overcome this limitation of FM sets, a two tube
transmitter was developed (Fig. 5). Variation in vacuum tube
resistance is used to modulate the oscillator plate voltage of
a self•excited oscillator in accordance with the audio signal.
This provides the freq,.1ency modulation desired. In order to
mainta~n a stable center frequency and render the oscillator
insensitive to changes in snpply voltage, a neon tube voltage
re~1lator was included.

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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.