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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…
(1) W : Balloon Volume x Gas Lift
Gross Load ·
[It may be noted from this equation that a balloon can float at
molar volumes less than that compute~ for maximum balloon volume
(i.e., when it is not full). However, under these conditions the
balloon would be in neutral equilibrium, since any vertical force
would cause it to rise or fall until a force in the opposite direc-
tion stopped it. This is also the case with floating extensible
balloons.J
To convert from molar volume to equivalent altitude we must know
the pressure-temperature diatribution of the atmosphere in which
the balloon will float. Since it is difficult to obtain an
accurate distribution for each flight, the atmospheric model as
drawn up by NACA standards has been used. In general the error
obtained in using the NACA standard is not great, but if greater
refinement is desired, date. obtained from averaged radiosonde ob-
servations over a given launching site can be used.
From such knowledge of the distribution of pressure e.nd temperature,
we may plot a curve of molar volume vs. altitude by use of the
following equation:
(2) 1013.3 mb
P1
By use of such a plot we easily find the floeting altitude of a
full non-exter.sible balloon by use of equation {l) to find molar
volume, and then of the plot of equation (2) to find altitude.
The two equations have been combined and graphed in. the form of
an altitude vs. gross load chart with helium &s the lifting gas
for various balloon sizes and verious release sites in the
"Operations" section of this technical report (Part II, page 108).
For the NACA standard atmosphere we may derive an equation for alti-
tude sensitivity by use of the molar volume-altitude relationship.
This is most easily done by plotting molar volume vs. eltitude on
semi-logarithmic paper, since the curve of molar volume vs. altitude
from 40,000 to 105,000 feet (where a constant lapse rate of zero
is assumed) is approximately a straight line on semi-log paper.
The general form of the equation for this portion of the atmosphere
is y =aebz where y is the molar volume and z the altitude.
It is possible to determine empirically the constants a and b.
For example, using the molar volume at 50,000 feet, we find from
*359 rt3 =Molar volume of air at standard conditions {273°K, l atm. pressure)
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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.