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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…
Since the back pressure forcing the helium out of a
full balloon When it is rising is 4 times as great at
1000 feet per minute as at 500 teet per minute, the rate
of rise is critical when an appendix is used. It has
been found necessary to limit the rate of rise to 700
feet per minute to prevent bursting at ceiling when using
General Mills 20-foot balloons with standard appendix.
It is believed, from laboratory tests, that use of the
spring bow stiffeners on the new appendix will permit rates
of rise up to 1000 feet per minute. Flutter in the bal-
loon fabric while rising is apt to cause failure due to
ripping at speeds of more than 1000 feet per minute. A
20-foot General Mills balloon will burst with an internal
pressure of 0.014 psi., which is about 1mb., equivalent
to a 200-foot rise at ceiling with a closed appendix.
III. EQUIPMENT TRAIN
A. Lines and Rigging
Following rigging failures early in the testing program,
careful study was given to the lines and rigging methods
used to attach flight instruments to the balloon. For
safety in launching, a factor of 10 to 1 is used on all
loads. Thus, if a 40-pound load is to be lifted, it is
not safe to use less than a 400-pound tested line. The
line strength should be determined independently if
possible, since the actual breaking point of lines runs
between 50 and 70'/o of the manufacturer's rated strength.
Braided or woven nylon is recommended for all rigging.
A stranded or laid line is subject to untwisting in flight,
twirling the suspended instruments and reducing line
strength. The nylon material is weather resistant to a
high degree and tends to stretch under shock rather than to
snap. For some purposes it may be desirable to use a line
of constant length, in which case the nylon may be pre-
stretched. Only a few of the common knots are useful
in tying nylon. Bowlines and square knots have been found
to slip and are hard to untie. The carrick bend, shown
in Figure ~is recommended. ln addition to this, a safety
knot is made in the loose end, and the entire tie secured
by a final taping. For convenience in assembly, the indiv~
dual pieces of line and equipment are rigged with harness
snaps at each end. This permits unit replacements or re-
moval at the last minute with a:t minimum of delay. For
extremely light-weight rigging, wooden toggles and loops
in the nylon may be used instead of the heavier metal
snaps.
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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.