On Sun, 23 Oct 2011 17:55:32 -0400, STEALTHMAN <stealthman@iglou.com>
wrote:

    Page Three,  Application 972527 - Continued 

11   Combinations of any of the above surfaces may be
       combined as long as
12    the unmodified straight lines or the straight lines
        after modification
13    are all in the same plane or all being perfectly
       parallel to one and 
14   the same arbitrary imaginary plane surface so
        that the reflected beam
15     from all surfaces falls or is projected as close to
        the other reflected 
16    beams from the same craft and all covering the
       smallest area possible,
17    so that the concept of the invention can be
        realized.

                              (8)

18   To illustrate the relative effectiveness of the various
        surfaces,
19   they might be assigned class numbers, with the 
       smallest number designating
20   the most effective avoidance surface configurations.

21   Class 1.,  Rigid surfaces which are CONCAVE,
        PERFECTLY SPHERICAL, highly
22   polished, with a radius of curvature of twice the
       maximum operating
23   altitude of the aircraft, or a radius of curvature of
       infinity for
24   spacecraft.

25   Class 2.,  Rigid surfaces which are CONCAVE,
       PERFECTLY CYLINDRICAL,
26   highly polished, with a radius of curvature of twice
       the maximum
27   operating altitude of aircraft and a radius of curvature
       of infinity 
28   for spacecraft. 

29   Class 3.,  Rigid surfaces that are flat, plane surfaces,
       with care 
30   taken to make sure there is no convexity whatsoever,
       or, concave 
31   surfaces which have a radius of curvature of infinity
       or near infinity.
32   Class 4.,  Rigid surface configurations that are perfect 
       cones, with
33   the straight lines modified to CONCAVE, highly
        polished arcs which
34   make up the cone itself and having a radius of 
       curvature of twice
35   the operating altitude of the aircraft, and with a radius
       of curvature
36  of infinity for spacecraft, and, perfect cylinders which
       have the
37   normally straight walls modified to become arcs that
       are CONCAVE,
38   highly polished, with a radius of curvature of twice 
       the operating
39   altitude of the aircraft, and, with a radius of curvature
       of infinity
40   for spacecraft.


             Page Four,  Application 972527 - Continued 

01   Class 5.,  surface configurations that are PERFECT
        CONES, and PERFECT 
02   CYLINDERS, and PERFECTLY CONICAL SECTIONS,
        and PERFECTLY CYLINDRICAL
03   SECTIONS, that are highly polished and _WITHOUT_
        any modifications.
04   Class 6.,  Combinations of any of the above, with an
       effort made to
05   cause all of the reflected beams of electromagnetic
       energy to fall, 
06   or be projected, directed, or focused, into as small
        an area as possible
07   so that the natural motion of the aircraft  and the
        relative size of 
08   the small resulting reflected beams to the large
       expanse of the 
09   Earth's surface under a 90 degree cone which has
        the aircraft at
10   it's apex, to cause the probability of said beams 
       falling or striking
11   on the receiving antenna of electronic detection
        equipment to be 
12    quite small, and if it does, then the amount of time
         that the beam
13    is striking the antenna will only be an instant and
        will probably
14    only occur once and will not allow any information
        about the speed, 
15   altitude or direction of travel to be ascertained.

                                      (9)

STEALTHMAN