“small beings”49 pages
- p. 17 …Others remain nonbelievers or
at least skeptical of the existence of alien beings and elusive vehicles…
- p. 19 …Moreover, operational necessity required that these balloons be launched during daylight
hours. It was therefore not…
- p. 30 …This has since grown from a minimal amount of debris recovered from
a small area to…
- p. 35 …This included, for example, a small
amount of missing "decimal files" from the 509th Bomb Group…
- p. 36 …This was a small section of the July Historical Report for the 509th Bomb Group
and…
- p. 37 …To believe that such operational and high-level security activity could be
conducted solely by relying…
- p. 39 …The foil-rubber material could not
be tom like ordinary aluminum foil can be tom... "
Sally…
- p. 40 …Although there does not appear to be much dispute that
Cavitt was involved in the material…
- p. 43 …Lt Col Cavitt described a small area of debris which appeared, "to
resemble bamboo type square…
- p. 72 …being per:ormed on these bodies.
The bodies were described as the body of a small…
- p. 99 …It should be noted that the period from approximately 1946 to 1950 is the least well…
- p. 105 …Several small projects were completed during ~1e mont.~ includine
signs on all the·office doors, a…
- p. 149 …Streett 1s
office recaumends against it on the ground that that is a
small enterprize down…
- p. 159 …I do not recall the incident being mentioned again as being any big
deal and I…
- p. 201 …We even simulated a small lightning strike over dry snow (just
from the snow blowing over…
- p. 258 …Big plastic
balloon with small auxiliary plastics," etc. "Watson Lab and
gear." "Followed" (inaudible) "receiver until…
- p. 261 …explain bodies or material that can't be
folded) by a sledge hammer.
Q: Let's…
- p. 328 …The witnesses have recalled small pink/purple "flowers" that appeared I to be
some sort of…
- p. 401 …b7 how ra*
the receiver •7 be re110ve~ .t'rows the pre~er. red height withqut…
- p. 443 …geostrophic wind (the latter being
derived under certain simplifying assumptions) and since the
geometry of the…
- p. 458 …Two designs which compro-
mise extreme cost (required for balloons of high internal pressure)
with small…
- p. 479 …This means that several hours might be required to fall through
the lanes of aircraft traffic…
- p. 484 …The change in drag effect may be realized by a decrease of
relative size of the…
- p. 487 (a)
Then:
(9)
or for small temperature differences:
(10) : - _L (.AI.)1-B T
the nega…
- p. 490 …gas of a balloon can be lost by:
leakage through small holes in the fabric or…
- p. 491 …for l:n•y small section of altitude is assumed
to be constant); and re.J…
- p. 506 in the preceding, section on diffusion end leakage the appendix
opening should be small. It can…
- p. 521 …is li~ited as indicated
above, small variations may be detected with the result
that it…
- p. 555 …being exposed about 10 hours
at cold temperature. (:S) During the floating period :many small oscilla…
- p. 565 …The very usef.ul information about be.llast flow was reported clearly, and
the principle of…
- p. 566 …Since the small external appendix with cardboard stiffeners was not
suitable for the large balloon, a…
- p. 580 …Following the initial activation at about 38,500 feet, small oscillations were
introduced into the flight…
- p. 614 …Figure 4 shows this appendix construction on a General M lls balloon which
is being inflated…
- p. 652 …At high altitudes, a difference of 40°C may
be expected in the temperature of the…
- p. 658 …To facilitate handling of the
line segments each length is prepared with a small hook on…
- p. 672 signals may be arranged so as to consume a very
small portion of -transmission time.
D…
- p. 738 …These values may
be compared with a diffusion loss of lift of the order
of magnitude…
- p. 742 …The constancy of level will be better the lower the
diffusion and the lower, therefore, the…
- p. 762 …te
.::mrcht:.se of small item£. A furth..:r rec:uest ~s been subr:rl tte…
- p. 783 …be of such a valve that
with a large r~diosonde frequency variation for a small…
- p. 785 …It is expected that this
equipment will be flown about 8 l-1ay. A description of…
- p. 815 …Before gear could be recovered, most of it had be~~tolen. Stations operating
at north hanger…
- p. 842 …Range started to slowly increase as did elevation with azimuth being
stationary. The echo remained beyond…
- p. 862 …By using this
stressed tape design, much larger loads may be carried than
the thin polyethylene…
- p. 874 …At this point, two small holes about
18" apart have been made, and the rip line…
- p. 881 …If thodolite stadia determinations are being
made, the banner can be used as one of the…
- p. 898 …laid out, A small amount of gas at very low pressure
Should be valved into the…
- p. 910 …The motor gears may be cleaned with
carbon tetrachloride and a small clean brush.
If the…
- p. 918 …Each combination of dots or dashes may be identified
by ear, and with a calibration chart…
Permission to use the MPS-6 in tracking further V-2 missiles having
been received, plans were formulated for operation in conjunction
?lith the missile scheduled to be fired Thursday, 22 July and post-
poned until Monday, 26 July at 1100. Plans contemplated that the
crew on the M-2 Optical Tracker would track visually at all times
during the flight with their elevation and azimuth readings repeated
on the antenna. The MPS-6 antenna was initially positioned in azi-
muth on the calculated bearing to the launcher and raised slightly
above the horizon in elevation, with the correct range gated on the
scopes and with a velocity of about 300 MPH set in the aided range
motor and the motor initially stopped. It was further planned that
when target echo would bloom on the scopes, the echo should be
trued up in Azimuth, Elevation, and Range; and antenna control would
be thrown to automatic with range followed manually until speed of
the missile approximated the 300 MPH as set on the motors, at which
time the video motor would be activated and range tracking thrown
to aAided." It was planned to throw antenna control to the M-2
Tracker only if target failed to show or if extended "loss" subse-
quently occurred.
During the half-hour period prior to the take-off, several random
aircraft were noted in the vicinity of the launcher; and at X-5
minutes, one low flying aircraft was observed on the scopes at a
range beyond the launcher directly in line with it and flying in
towards the launcher.
Timing signals and the zero signal were received, and at about
X plus 2 seconds the target "bloomed" on the J Scopes at the cal-
culated range to the launcher (62,800 yards). This pip went almost
instantly to far beyond saturation, and all grass disappeared from
the scopes. The Azimuth and Elevation, and Range controls were cen-
tered on the target, and antenna control was thrown to automatic.
Range started to slowly increase as did elevation with azimuth being
stationary. The echo remained beyond saturation for about two sec-
onds after automatic control was thrown in, at which time grass ap-
peared on the scopes and the signal fell rapidly to zero and the an-
tenna whirled off target at about X plus 6 seconds. Upon returning
antenna to position manually, a strong target appeared at a range
of about 2K yards outside ~he range gate, and believing this to be
the rocket, this pip was trued up and antenna locked in "Automatic"
and this target was tracked for a period of about 10 seconds or
until it v1as noted that range was decreasing and elevation was sta-
tionary at the horizon while the M-2 Elevation repeater showed the
optical tracker to be looking at approximately 50 degrees. Realiz-
ing that the target being followed was the aircraft noticed before
take-off, antenna control was transferred to the optical tracker
and left in its control until the M-2 crew lost the missile. During
this time, no target was visible at any time and no further radar
contact was made with the missile. However, slightly before the
missile impact wao beard, a cluster ot small echoes were found at a