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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…
1,3.
D. Launching Services
During the course of the project balloon .flights were split into·
two general classifications, (a) research and (b) service.
Research flights were made to test balloon contrOls and telemeter-
ing systems developed under the contract.· A .tul.l report of these
research flights has been mac!e 1ft "Technical Report 9.3.02 1),
Section lii, Summar,r of Flights•
Service fiights were carried out by New York UniTersit7 personnel
in conjunction with technical personnel from the sponsoring ageney
to test geophysical equipnent deTeloped in Air Force laboratories.
The requirements for these fiights wre launching and tracking
of balloons to float at specified altitudes for short periods of
time (6 to 8 hours). Because of this short .tl.ight ·duration,
simplified plastic balloon STStas wre used. Balloons were
maintained aloft by ,,se of constant fixed ballast now, or ballast
was excluded entirely from the 87Stem. A typical night using
constant ballast flow at a rate slightl7 exceeding leakage losses
is shown as Fig. 8.
i-
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t.•
J...
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I
,. I I I I I 1 I I I l
I I
t-i. /'
I
11\ \ \ v i _\. \ .\ ... l. 1 . \ ~
1100 1100 a: 0100 otOO ~00 0100 1000 1- 1100 1100 1400
T••e-MIT
NYU BALLOON PROJECT FLIGHT 82
Barograph Record Of G.M. 20' Pla1hc Balloon W1th
534 gm/hr F1xed Balla1t Leak
ltiLIAUD AT ALAMOIOitDO,N.M.- OIIIMIT, 10 AUI 1141
DIIOINDID AT ltOIWILL,N.M.• 1110 MIT, 10 AUI 1141
DURATION• ill lite
Fig. 8
Balloon Flight Using Fixed Ballast Flow

Cases discussed

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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.