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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…
F~OJECT ABSTTIACTS
Chief: Dr. James A. FeoJ;le.i • ..::::-.
1. Fro.1e:~t tit-le: A.~ol.4s"L: ~ounaing of the Atmcspbe:r-e
f':roject. sdentist.:;: Dr. :. A. i'eople:3, Jr., Dr. i•lor:ua.n
Haskell
Summary cf In-Laborat.:'lry ;·,ork:
'When large explosions i1av-;' o>!curred, it J·.as been observed that the soWla was
heard locally, say up to ::5 mile:s, and als.:> at dbtances of 100 to 200 miles, but
that nothinf; wa:; reard at intermediate distan~es. This phenomeru11can only be
explained by assumjng that the sound ts refracted into ths atmosphere over the 1n-
termedi2te observers and then is bent back down to the ;nore distant areas. For t~ds
to occur t.ho velocity of propagation must first decrease with altitude and then
increase &!&in to a value at least as lar~e a3 ground velocity. this is due to a
decrease of temrerature up t.o the tropopause followed by an increase in temperature
above that level. V:inds also have an appreciable affect which can be determined
from asymmetrical propa~ation.
Up to abo~t 1946 most data on this phenomenon had been obt&ined by taking
polls after accidental eaplosions had occurred. Zones ot audibility were mapped out
and ~ener.al conclusions then drawn. Very lit.tle systematic w·ork was done in \Which
accurate travel tiAs and other factors were obtair.ed. Beginning in 1~46 at these .
laboratories, a systematic study of these pr"p~at!on anomalies were started. Sound~
ran5ing detectors ware set up in arr&Js, so thsarvations h; "te bec!n tG.k6b ih the vicinity of Fairbanl:s• Alaska for in!or.." t on o.t
~.I"i J.igtj latitud~s4 · Ob~er.vatj,.dn,; .ha•e been taken near the Panama Carial Zone for
~:ci~Uiional information i.i1 tbt: !r#i.csi
The sounds produced by rockets launched a\. .k..1ar.togordo have been recol'd~d .~ith
acousti= detector arrays located on the gro1nd neer the rocket trajectory. From data
gath-=red in this nt£11Iler, soraa inoic~ ti.m!:' of apper air te11.par~tl.lre a."lU .viud::> Lo.ve ween
obtained and much :no:e accurate date:rm.im. tion:; could be ;,lade if U1Q rock~t trajectories
were more accurately known.
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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.