“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…
Flight 17, using a fifteen-foot balloon of .004 Polyethylene is
worthy of special consideration. The thickness of this type of cell
eliminates much of the problem of appendix design since more internal
pressure can be withstood. Despite this factor, and the low permeability
of the fabric, balloons of thie type are too heavy and costly to be used
for higb altitude flights.
The trajec.tory and time-altitude curve of this flight are shown
in figure 56 and 57. This controlled-altitude flight demonstrates that
the automatic ballast valve combined with a fixed leak, will successfully
maintain constant altitude through a sunset. The balloon floated at 29,000
feet + 500 feet for at least three hours, after which the excessive range
prevented further radio reception. Here again the necessity of a barograph
was demonstrated as the balloon was recovered from Pratt, Kansas, 530 miles
away. Two flights, 23 and 38, were made using the shrouded Dewey and Almy
J-2000 Neoprene balloon. Both of these flights were failures. Flight 23
(see figure 48) attained a maximum altitude at 50,700 feet and began to
descend immediately. Flight 38 (see figure 55) was observed from a B-25,
and the balloon was seen to burst ld thin the shroud.
Section 6. Current Objectives
In order to meet the requirements for future flights, improvement
must be made in three phases:
1. Performance data for too many flights have been either uncertain
or of too short duration. Before more flights are undertaken,
altitude~easuring instruments must be improved and increased.
To this end, four specific improvements are being ur.dertaken:
A. To supplement the pressure data received by r~dio, a
lightweight barograph will be added to those fli~ht
trains in the future when fli~ts of more thfl.n e. fow
hours' duration are attempted,
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