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…
When the total quantity of gas needed has been computed,
the lift requirement may be expressed in terms of the
pressure of a number of cylinders of gas. It is not
possible to assume that each tank of gas will give the
same amount of lift, nor is it possible to use a gage
which has not been expertmentally calibrated to relate
lift to pressure. For calibration of a gage it is suffi-
cient 'eb valve gas from an observed equilibrium tempera-
ture and pressure in a cylinder into a rubber balloon
8:ll4 then measure the total lifting capacity o! the gas
from the tank. Check points should be made with tanks
under varying amounts of preseure. Figure 19 shows a
sample gage oalibration worked up for varying temperatures
auUJiling the simple gas law
Lift2 : ..£2._){....!1_ Lift1
pl 1'2
This law applies to w1 thin !1%. Note: Do not use Graph 6
without checking calibration of gage to be used. Ordi-
narily a whole number of full tanks of gas will not
exactly supply the desired lift,which should be figured
with not more than one-tenth tull tank tolerance in ex-
cess (penni t no under inflation). It is thus necessary
to prepare partially full tanks and by combining full and
partially full cylinders get the required total. It is
necessary to allow the cylinders to attain equilibrium
temperature after valving them before taking final pressure
readings.
B. Length of Balloon Bubble
The volume of gas required for a given balloon may be ex-
pressed as the length of an uninflated bubble at the crown
of the balloon. Graph 2 of Appendix II gives the relation-
ship between bubble length and resultant inflated volume,
using gross lift as an expression of volume. It will be
noted that when the elevation of the launching site is
markedly different from sea level, a shift in this curve
is needed to accomodate varying densities of the atmosphere.
The inflation of this bubble, which is pinched off by
launching equipment or shot bags, will serve as a good
check of the final amount of gas in the balloon, thus
warning if the balloon is underinf'la ted.
c. Expected Altitude
To predict the altitude to which a balloon will rise it
is necessary to know the volume of the balloon, the total
-33-

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.