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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…
its bursting diameter, the gear strikes the ground, or corrective
action is taken. Even if the extremely critical balance is intially
achieved, there will be 'Imbalance occasioned by (1) bursting of
balloons due to deterioration in the sunlight, (2) diffusion of
lifting gas from the balloons, (3) loss or gain of buoyancy "'hen
temperature inside the balloon changes with respect to the ambient
air temperature. This will result initially from radiative dif-
ferences, and after an amount of difference (superheat) has been
established, changes in ventilation will cause changes in buoyancy.
Two methods of attaching the payload to the clusters of rubber bal-
loons were tried. In the first of these (Figure 3) a long load
line was used,and short lines led from it to the individual bal-
loons. The length of such arrays was as much as 800 feet, and
this size made them difficult to launch. The single load ring
array, seen in Figure 4, proved to be much easier to handle and
is recommended for cluster lfnmchings. During ascent each of the
balloons in such an array ride separated from each other and no rub-
bing or chafing has been observed.
The controls which were associated with this balloon system were
crude and, in general, ineffective. They included (l) cutting off
balloons as the buoyancy became excessive and a preset altitude
extreme was passed, and (2) releasing part of the load in the for.m
of solid or liquid ballast whenever descent occurred. The sensi-
tivity of these elastic balloons makes it difficult to control
their altitude with any system of controls, and as controls were
developed it was found more practical to change from freely ex-
panding balloons to non-extensible cells not made of neoprene. The
tendency of neoprene to decay within a few hours when exposed to
sunlight was the most cogent argument against doing more work on
altitude controls to be used with such a system.
B. Plastic Balloons
The next attempts to control the altitude of a balloon vehicle were·
made using non-extensible plastic cells, with an open bottom to pre-
vent rupture when expansion of the lifting gas is excessive. With
a fixed maximum volume, such a system has inherent vertical insta-
bility in only one direction. When full, there is· e. pressure alti-
tude above which a given load will not be carried. The instability
of such a system is found only when an unbalanced d~nward force
exists. The development of controls and films for balloon material
proceeded concurrently, but the choice of a.non-extensible plastic
film was made before the system of control was perfected.
The properties which were given most consiaere.tion in the selection
of fabric include (l) availability and cost, (2) ease of fabrica-
tion and (3) satisfactory chemical and physical properties. Pri-
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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.