Documents / FOIA release

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…
td (d 'where 2.1t> !!A_} is the- time during which pressure change of
the airdlurro8h!1~g the balloon is greater than a design value
of pressure change causing ballast flow.
The general equation, then, indicates the relationships between
the variables involved in balloon flight. The discussions in
this section of the report, "Equations and Theoretical Considerations,"
attempt to qualitati~y organize the relationships between these
variables in order t~.t a complete overall picture of the aspects
of balloon flight can be formulated.
It should be stressed that the theoretical relationships as stated
here do not lend themselves to simple insertion into an overall
equation which is easily solved. Rather, solutions .of marv of the
variables are ~n themselves complex. At this time it appears im-
practical to delve too deeply into such matters as "the variation
of diffusion and leakage through various types of balloons under
different conditions" or "a study in the change of coefficient of
drag on a balloon system at all points during its flight." It
has been rr:ore practical to generally state the relationships in
unsolved form and concentrate the experimental portion of the re-
search problem on such :me_tters as actual development of balloon
controls.
V. TELEMETERING
A. Information Transmitted
The need for a balloon-borne transmitter and some system of ground
receiving and recording was recognized early in the ~ork of the pro-
ject. The primary objective of such telemetering was to collect
data to evaluate the altitude controls applied to the balloon sys-
tem. Pressure, perhaps the most irr:portant data, was measured by
the use of radiosonde-type aneroid capsules. A discussion of the
pressure modulators used is given in the following section.
A second use of air-borne transmitters was to provide a beacon for
radio direction-finding. With proper equipment a balloon-borne
transmitter can provide a signal to guide an aircraft, homing with
a radio compass, or provide a position "fix" by the crossed azi-
muths of ground receiving stations.
In addition to these two very important functions of altitude
dete~.ination and positioning, telemetering systems were used to
detect and transmit temperature data and ballast flow data. The
equipment used for these purposes is described below.
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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.