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. 224 …But I think this was trying to chase Flight 8 down. This was one of the…
  • p. 256 …As long as we could end up with that very expensive aircraft chasing an air balloon…
  • p. 268 …Here's a letter Todd got having to do with chasing down modern targets, the people…
  • p. 475 …gation of commercially .sold chambers showed that the c.ost of pur- chasing a temperature chamber…
  • p. 771 …Advising NYU still interested in pur- chase of balloons. Requesting tha.t in- spection date be…
  • p. 801 …Caught 710 train to NYC, cashed check at Chase Natl Bank, talked to :!!:wing on phone…
of displacement switch actions alone.
...0
:::>
...
IF LEVELING OFF TOO LOW, H.IGH
BALLAST RATE PUSHES BALLO.ON
INTO CONTROL ALTITUDE.
CASE "A"
, ~;;;-"' ~ -- -- -- -- -- -- -- ---- - -
... -~TOOL~' -- ,..-, ,--..
~ -~ASE "a"---.;;..;._~--
IF LEVELING OFF TOO HIGH
----- ---- _ _Lw:!BA:~A~T-U~T~ TH~~!~ME.
I ______l ____l ____ I ______ I_---=~~---_-
NORMAL 8ALLAST FLOW- CASE "A"
~~---------------~=-~~~~==-----:~:.:To~:l'i.L:~~SE aAI.!,AST FLOW- CASE "a" !RATE SWITCH FAILUREl-
TO INDICATIE PROPER
CONTROL ACTION. (!) PEN OFF SHELF
TIME
@ TOP LOW ALT. COMMUTATOR
@ aOTT. HIGH ALT. COlliN.
Figure 15. Theoretical height-time curve.
(4) Rate-of-Descent Switch
It may at times be desirable to control a balloon merely qya
switch activated at any given rate of descent. This could be
accomplished merely by "reversing" the rate-of-ascent switch.
This type of control would prove to be quite difficult, however,
for a constant level flight. One flight, No. 97, was made
using a type of rate-of-descent switch ·&s shown in Figure 16. In
...---------------------------------1
I
I Pos1tron whrle-,-~--------
rrsrng ..: ----------
1 AdJustable \_ Posrtron whrle
I Contact --...... ---, Descendrng
I I
I !I
L __ _ ' Ballast I'\_Solenard 1
1
Valve !
I I
L_~'l'l'l~~
Sealrng Valve
(Actuated at
de11red altrtude)
Figure 16. Rate-of-descent switch.
Coprllory
Tube

Cases discussed

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.