ERV SESSION PROCEDURES REPORT CONTROL NUMBER: 8709, SESSION NUMBER: 04, SOURCE IDENTIFIER: 003

• Document Type: CREST
• Collection: STARGATE
• Document Number (FOIA) /ESDN (CREST): CIA-RDP96-00789R000300590001-4
• Release Decision: RIPPUB
• Original Classification: S
• Document Page Count: 13
• Document Creation Date: November 4, 2016
• Document Release Date: June 22, 1998
• Sequence Number: 1
• Publication Date: August 20, 1987
• Content Type: REPORT

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OMOMMW/NOFORN --SKEET CHANNELS ONLY
PROJECT SUN STREAK (U)
ERV SESSION PROCEDURES REPORT
WARNING NOTICE: INTELLIGENCE SOURCES AND METHODS INVOLVED
CONTROL NUMBER: 8709 NICKNAME:
DATE OF SESSION: 20 Aug 87 TARGET COUNTRY: UR
REFERENCES: None SESSION NUMBER: 04
DATE OF REPORT: 24 Aug 87 MISSION STATUS: Continuing
TECHNIQUE UTILIZED: ERV SOURCE IDENTIFIER: 003
1. (S/NF/SK) INTERVIEWER TASKING: Tasking as listed in the
previous sessions conducted with this Source on this project has not
been changed or re directed. This session was concerned with Phase
II of the tasking package, the description of the characteristics and
configuration of the Soviet prototype/counterpart to the US "Stealth"
bomber. Other phases of the tasking package were not addressed in
this session.
2. (S/NF/SK) SOURCE TASKING: Source was told this was a
continuation of the last session and that He was to continue to focus
His attention on the unusually configured aircraft that He reported
on in His previous seSSion. In addition, Source was provided the
same encrypted coordinates as in the previous session, 137500/112794,
as per Extended Remote Viewing (ERV) protocols.
3. (S/NF/SK) INCLEMENCIES: Source was told just prior to the
beginning of this session that it would be conducted utilizing ERV
protocols. Source has aot received formal instructions in the ERV
technique and this was therefore a sudden departure from His normal
procedures (Coordinate Remote Viewing CRV) and the first time that
this Interviewer and this Source had conducted a joint ERV session.
Source is a very flexible individual and after only a few moments of
pre instructions, He was prepared to begin the session and did so in
what seemed to be a productive and in an altered state of
consciousness conducive to good Remote Viewing. There were no other
inclemencies or anomalies which may have affected the data provided
by this Source.
4. (S/NF/SK) SUMMARY: Source furnished the attached summary which
was prepared following the session and submitted to the Interviewer
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sOMMIPMA/NOFORN - SKEET CHANNELS ONLY
within 24 hours after the session. The completeness of the
typewritten summary has been compared to the Interviewer's notes and
all omissions, changes, and/or corrections have been verified as
acceptable by the Interviewer. The information provided in the
summary was found to be complete and did not require further
modification, clarification or additions by the Interviewer. Source
did provide some very detailed post session sketches which are
attached to this report +or reference purposes.
5. (SiNF/S(::) COMMENTS Source's initial foray into the ERV
protocols seemed to be on the surface as successful as His excellent
reporting record in the CRY methodology. In future sessions, the
focus of attention will be on Phase II, the comparison of the US
Stealth to suspected Soviet prototypes. At that time Source will he
utilized in the CRV mode until He become more comfortable with the
ERV technology.
SG1J
Interviewer
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Aircraft in question slopes..up-from_taj.1 to nose rear of
aircraft is very close to ground where it sits. Its nose has
some bulges or "lumps" to it, has curves and flat areas, and
doesn't come to as sharp a point as one might find in other
similar aircraft. From the front the body has a .":?lat, sgbished"
appearance, making it wider than ?usualN serves_some-sOrt of lift
+unction. Aircraft is dark in color . dark grey-green and dark
grey-brown, in a slightly mottled pattern. Paint texture is very
matte--a0nost porous and rob6h. ?:.AOL highly suggestive of
stealth-type fighter. Few or no acute or sharp angles. Body
elements ..... -wings, stabilizers, air intakes, canopy merge smoothly
and apparently seamlessly into the fuselage. Canopy/cockpit area
Si. sn't as rounded as in other planes faceted, not so much glass,
smaller viewing area. Maybe more than one. person Carried by the
aircraft, perhapide by sI de', Symmetrical top and bottom, not
side to side. Body flares out, edges are roUnded, with very few
or no sharp breaks. The wing sweeps and curves back. It is
"supercritical" to cut down on turbulence, friction, signature
noise. Signature no is detectable, draws at indicates
passage. Wi.ngs,-curve downward somewhat, more towards end- hard
to tell where the wing ends and body begins, or where the tails
attach. Wings bulge with a thicker part at the end. At the back
where the wings join the tail area, they flare downward somewhat.
There are two enginet, "ducted fan", internal, quiet_engines;.
high compression, cool what comes out_js Codler-than-Standard.
There is an iris-like? thing at the back of each engine that opens
and closes as necessary. The aircraft has black boxes,
electronics. One thing looks down, all?around, underneath.
Another involves countermeasures, frequency, radiation'patterns.
Another black box involves navigation, AOL terrain following
I' adar. The next is behind the cockpit area ..... -seems like IFF.
There is also a micr'bOF6-&66r that helps fly the aircraft. All
these things are tied together somehow.
Other side doesn't know about this aircraft -it takes
advantage of weaknesses in protection systems, looks .f: or niches
in where system doesn't perform so well. It likes to be low,
goes in between things instead of over them part of Si.
P rotection is its ability to do that. We are inside. Not
many of these aircraft, perhaps its a trial model or a prototype.
It can no a long ways and is pretty big. Very state of the art,
like anything new that might be useful has been put into it.
There may be something unusual about -the slant of the wings .....
they may slant forward, or downward more than usual, or
something.
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Project: 6499
Date- 20 av9eLL7
Sessi n: 03
Source- OOr))
Coordinate:
Page 1
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