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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. 539 …Too muoh weight was lost in this action, and the train rose until aome of the…
  • p. 540 …Train, Flight 10 The balloon rose to about 16,000 teet MSL and dropped back to…
  • p. 554 …It will be seen that the balloon rose~ a ' .. --------- r- ....., ..:. Pon"'m j"'.,.._" k '~I I…
  • p. 572 …obtained, but during this time the balloon rose with predicted speed (500 feet per minute) nearly…
  • p. 585 …On the other hand, the balloon rose extremely slowly and may have taken in air to…
  • p. 665 …In flight 7, however, the cluster rose till the lifters were cut off, descended until sufficient…
  • p. 739 …As a result, the cluster rose to ceiling and stayed at this altitude for a short…
  • p. 786 s4cond cluster flight, provision was also made to release balloons if the train rose above 40…
Flight 97: Released from Alamogordo, New Mexico, 0856 MST, September 10, 1948
Recovered at Duncan, Oklahoma
On this flight a .001", 20-foot polyethylene balloon was used to test a
new type or ballast·control. In this system, ballast flow was excited at any
altitude if the balloon descended at a rate equal to or greater than l milli-
bar in five minutes.
The buoyancy record and the Olland-cyole pressure data obtained from this
flight show a disagreement of about 10,000 feet (Figure 45). No explanation
has been provided for this difference and the following evidence has been
considered. 'lhe predicted floating level was about 45,000 feet, in agreement
with the Olland-cycle radiosonde data. On the other hand, the balloon rose
extremely slowly and may have taken in air to dilute the lifting gas. In this
event, the floating level Jr.ight easily have been reduced by 10,000 feet·.
40 .J
=I
i..
tO
1t
10
~ /
0
oeoo 1000
OLUND C'I'CI..E a.la
~ ....--- I ---
"I ~ TRACE llllla
---· ---- ___ .,. ______ [_ ----- -...... -- .../----- -- I I ' ' .
jA .
FUGHT 97 '·
,I I Raleased at Aklrnogoldo,N.M.!
I I Sept.IO, 1948- 0856M.S:T.
I RecxMred at Ouncci\Oicla.
--f---- ~-
1100 1100 1100 1400 1100 1100 1100
.,.. (IILS.'t)
Figure 45
Once at the floating level, however, the balloon ?.'8.S maintained within
1000 feet (or 1200 feet) of a constant level for over four hours. This in-
dicated that the control system was in operation since previous flights
{88 and 93) at this altitude descended after about two hours of flight with-
out ballast.
-56-

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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.