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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…
radar station was not tro~bled by this phenomenon due to its an-
tenna directivity and elevation orientation o£ 60 degrees. It is
believed that the intermediate loss or signal by the radar station
is normal because or elevation pattern lobing produced by ground-
reflection interference which is initiated by secondary antenna
lobe transmission. Since this condition exists in the transmit-
ting pattern, it affects both the radar station and its remote re-
ceiving station. Current effort is concentrated on improvement
of photography and antenna orientation in preparation for addition-
al tests.
b. Tracking Projects:
(l) Radar Tracking Set AN/MPS-6 • A letter was received from Watson
Laboratories authorizing changes and modifications of the range
circuits necessary for conditions as encountered at this location.
The fore part of July was spent in achieving these betterments,
and in the installation and orientation of an M-2 optical tracker
to be used in conjunction with the KPS-6 and as a tracking aid.
Experimental tracking of three balloons furnished and flown by the
Atmospheric Group was performed for the dual purpose of checking
the signal return of the radar with various reflecting targets,
and for precise position data of the balloon equipment for use by
the Atmosphe~c Group. On 19 July, a 130 toot balloon carrying no
radar reflector was tracked. Radar contact was made at a range of
about ;3K yards with signal return being above saturation on the
scopes of the KPS-6. Tracking was automatic in Azimuth and Ele-
vation and aided in range. Signal return remained above satura-
tion until a range of 7K yards was read, at which point grass ap-
peared on the scopes and signal to noise ~yeraged about 4 to 1
out to a range of 2JK yards where too frequent radar losses neces-
sitated that automatic tracking be abandoned. This balloon was then
tracked manually to a maximum range of 271 yards.
On 20 July 1948 1 a weather balloon carrying one kite type reflector·
was flown and tracked. Contact was made at a range or Jl yards,
and signal return was above saturation at all times until a range
of lOK was exceeded and grass showed only occasionally out to
~4,360 yards. This balloon was obscured by clouds at a range of
JJK yards, but tracking was continuous in automatic Azimuth and
Elevation throughout its £,light, and the maximum range read was
34K yards.
On 21 July, a lJO foot balloon, identical with the one flown on
19 July except for three kite reflectors being carried, was flown
and tracked. Radar contact was made at a range of 1,510 yards.
Grass first appeared on scopes at a range of 24.51 yards, and sig-
nal was above saturation to )OK yards. Tracking was continuous
and automatic throughout the flight, and a maximum range of 1211
yards was reached.
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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.