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…
If a balloon is teardrop in shape rather than spherical, the curve
would be modified so that the value of c0 , for a given Reynolds
number would be lower. In this case the sudden drop in C0
as Reynolds number increases (the change from viscous to turbulent
flow) would occur at a lower Reynolds number.
We have thus far in our discussion assumed that there is no verti-
cal motion of the air surrounding the balloon system relative to
the coordinate ! • However, this is not necessarily the case
under actual conditions. In many instances vertical llir movement is
found in the a bnosphere. Therefore, we must introduce a term to
allow for this vertical air movement. In equation (2) this term
was indicated as :tFA , the external atmospheric force.
We may consider this vertical air movEment· in terms of a velocity Dt.
Then the vertical velocity of the balloon system relative to the
air surrounding the system will be the difference between the velo-
city of the balloon relative to the absolute altitude Dt and the
velocity of the surrounding air relative to the absolute altitude
This may be equated as D~- 0 C , where Di and DC are both con-
sidered positive in the direction of increase of altitude.
The total force due to the drag, or friction will be:
FD + FATM: CD:. A ( 0!- oc>2
where the00otations are those used previously, exc.ept that now
NR = (Oz- :71 de • The relationship between NR and Co will be those
used previously.
The force due to buoyancy of the lifting gas F8 = Vb (P0 - Pg)
where:
vb: balloon volume (ft.3)
density of the air and lifting gas, respectively
(lb./ft.3)
This term my also be stated as:
where:
P0 , Pg = pressure
R0 ,Rg = specific
F
of air and lifting gas
gas constant of air and lifting
Ta, Tg : temperature of air and lifting gas
gas
The changes that will take place in this expression are those due
to a temperature difference between the lifting gas and the free
air, change in volume of the balloon due to loss of lifting gas,
change of the gas· constant of the lifting gas due to dilution with
air, and (in the case of a balloon that will hold an internal pressure)
pressure difference between lifting gas and surrounding air.
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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.