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.
“Gross”26 pages
- 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…
d. M~thods of Attack
(1) .4fter ~ survey of •;_vf.:.ilable literature in aerostatics £_r.d
after conferences with v&.rious balloon r.w.nU:ccturcrs [..ID Euthoritit:s it
is believed that th.s DG..sic problem cf ;:1£.intEining the 15 lbs. cf payloed
at constant altitude can test te solved ty using a non-extensible balloon
ani a device operatea by I-Jress'tll'e which drops ballast whenever the
balloon descends below a preset altitude.
The specifications for the equipment are ~s follows:
The balloon should be of large known volume, light in weight,
non-extensible, either transparent or highly reflective to
sole..r radiation. Rigging should. be used to O.istribute the
load evenly about the balloon.
A safety valve should be used to hold. the inflation appendix
of the balloon normally closed (as any hydrogen lost decreses
the time ;_Jossible at nominal constar1t altitude). The va.lve
would act as a safety vent if the balloon should rise appreciably
above the altitude where it is fully inflated, as there is danger
of rupturing the envelope unless the excess yressure is relieved.
The safety valve should be set to release ;>ressure before the
limit of the working stress of the balloon f~bric is reached.
If the eY.act volume of the balloon is known and the air density
vs. altit·u.de rele.tionship is determined on the 2.ay of i'light,
it is possible to compute the total lift of the gas in the
balloon at ~ny altitude. By adjusting th~ gross load to be
supported by the gas to equal the total lift at the uesired
altitude of flight, the balloon will level off at the datred
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About this file
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.