Documents / FOIA release

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…
levels when the instrument is located out of doors.
For details of the use and care of theodolites.
see either the War Department publication TM-11-
423 or the U. s. Weather Bureau Circular "O".
(3) Aircraft Radio Compass
It has been found feasible to deter.mine the posi-
tion of the balloon by following the signal from a
balloon-borne transmitter. using an aircraft radio
compass as rece~ving unit. In this way it is possible
to fly along a path coward the balloon,·usually at
a much lower altitude. and. by noting the plane's
position where the compass reading is reversed. the
position of the tra-nsmitter is found. The main dis-
advantage of using this system is that aircraft is
n~eded. but there is no other method which will so
readily position the balloon over great distances
and periods of time. With this system. the limit
of tranamission time is a function of the weight of
transmitter batteries which can be carried rather
than distance. It is possible to power a trans-
mitter to supply 2 watts. for about 15 hours. using
15 pounds (7 kilograms) of batteries. Longer periods
of transmission may be achieved by intermittent opera-
tion of the transmitters or use of heavier batteries.
(4) Radar
If ground radar is available, accurate pod tioning
over a limited range can be made. It is helpful
but not strictly required to add radar targets
(corner reflectors) to the flight train for such
tracking. Using radar. the elevation angle • azimuth
angle and slant distance out are obtained, giving
a complete fix on the balloon with one set. The
maximum distance to which appropriate sets can reach
is about 65 miles; such sets are the SCR-584, the
SPM-1 and the MPS-6. V'lith good orientation and leveling
such seta have an accuracy of l.oo and about 500 feet
of slant range. Because of the limited range, radar
sets are not generally useful. Attempts to use
radar mounted atop aircraft for aeri~l observation
have been abandoned in favor of the radio compass.
B. Altitude Determination
In early attempts to utilize standard radiosonde
pressure modulators they were found to be unsatisfactory.
The Diamond-Hinman system of counting signal changes
-53-

Cases discussed

About this file

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.