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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…
B. Transmitters Used
(1) 72-Megacycle Radiosonde Transmitter (T-49)
The standard T-49 transmitter of the Ar.my Weather Service was
first used in project work, with a modified commutator bar
switching specially coded resistors into the circuit. as the
balloon passed from one critical pressure to another. The
operating characteristics of this transmitter may be found in
the following publications: T.B. Sig. 165, T.M. 11-2403,
T.M. ll-2404 and the Weather Equipment Technician's Manual.
The defects which were encountered in the use of this trans-
mitter were principally (1) relatively short range and (2)
unfitness for direction-finding using available equipment.
Our experience has been that reception from the T-49 trans-
mitter by standard equipment is not much above 80 miles under
good conditions. lihen flights were made which traveled many
times this distances, the inadequa~y of this vransmitter was
clearly demonstrated.
The problem of direction-finding is of major importance when
attempts are made to position e.nd track the balloon and its
equipment train. Since no standard directional receive~ equip-
ment is available for this use with the T-49, this transmitter
is of limited value.
(2) 400-Megacycle F.M Transmitter (T-69)
The T-49 transmitter was abandoned in favor of the T-69 400-mc
system as soon as ground receiving equipment for the latter was
available. By using the directional receiving set SCR-658
with the T-69 transmitter, the problem of direction-finding
and positioning was attacked. A second advantage enjoyed by
this system is the improved range attainable.
Our experience has been that an SCR-658 set in good condition
can receive a signal up to a range of 150 miles, providing
that the line-of-sight transmitter is high enough to preclude
blocking by intervening terrain. The use of two or more sets
to increase the area of a tracking net is discussed under
"Radio Direction-Finding" below.
The operating characteristics of the T-69 system and the SCR-658
may be found in these publications: T.B. Sig. 165, T.M. 11-ll58A.
Pressure indicators were obtained, as with the T-49, by use of
the modified commutator bar switching specially coded resistors
into the circuit as. the balloon passed from one fixed pressure
to another. A few special tests were made of a chronometric
system of pressure modulation. For a complete discussion
of pressure modulation methods, see Section Vl, A.
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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.