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…
Position of recording and radio instruments in the flight
train is in some oases dictated by the size and shape of
antennae or other special part. In general this type of
gear is not placed below the altitude control equipment
because of possibl~ damage which might result from
ballast being dropped upon them. ~pical trains are shown
in Figures 16, 17, and 18.
F. Flight Tools and Equipment
A list of tools and equipment and facilities which should
be provided for any launching site is given in Appendix II.
IV. PRE-FLIGHT COMPUTATIONS
A. Lifting Gas and Rate of Rise
When the equipment for a flight is in readiness and the
inflation procedure is to be begun, the total weight to
be lifted must be determined. A weight sheet (Shown in
Appendix I) is filled in, with the final weight of each
piece of gear with its rigging. In this work the wei~hts
of the equipment are measured in grams and kilograms. for
ease of computation. The gross load reported should be
accurate to the nearest 200 grams. The amount of lifting
gas to be used must be carefully figured to prevent in-
correct inflation which might result either in the bal-
loon failing to rise, or perhaps rising too fast and rup-
turing at its ceiling. After the total weight to be
lifted is found, a percentage of this total is added to
provide for lifting the load at some specified rate.
With a given excess of buoyancy, a balloon will lift its
load at an almost constant predictable speed. (The rate
of rise will increase by about 25% at higher altitudes,
due to the changes in balloon shape and decrease of air
density.) Graph 1 of Appendix II shows the relationship
between the free lift and the :t-ate of r·ise, with free
lift expressed as a percentage of the total or gross load
(which includes the weight of the balloon itself). For
example, if a gross load of 10.0 kilograms is to be lifted
at a desired ascent rate of 600 feet per minute, 9.2%
of the gross load should be added, giving a gross lift
of 10.0 t .920 • 10.920 kilograms. (The rete of rise
should not exceed 700 feet per minute if a standard appen-
dix is used.)
It should be noted that this graph, derived from equations
for spherical balloons, applies also to the tear-drop cells
of General .Mills, Inc., without regard for the balloon
die.mter.
-29-

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.