“The Sun”32 pages
- p. 43 …to the sun for only a few days. The
plasticizers and antioxidants in the neoprene would…
- p. 205 …ashes after exposure to the sun for only a few days. The balloon material and radar…
- p. 221 …to the sun.
Q: Is this the neoprene type or the •••
A: That's the neoprene…
- p. 230 …such as
the balloon material degraded, and maybe fused in the hot sun?
14
A: I…
- p. 282 …We worked in the old Sun newspaper building in downtown Baltimore.
Q: They had intelligence personnel…
- p. 465 …the values of superheat ob-
tained by the gas when the balloon is in the sun…
- p. 484 …Superheat and Its Effects
The effect of the heatin~ of lifting gas by the sun's…
- p. 489 …Since the effect of the sun in heating the lifting gas decreases
the effect of different…
- p. 524 …when the ex-
ternal temperature was measured, since no adequate protection from
the sun was available…
- p. 525 …Daytime flights had the added advantage or heating from the sun.
The temperature of the lifting…
- p. 541 …in the aneroid
val~e as intermittent clouds shut off' the sun, and (3) the overcompensation…
- p. 547 …stmset, and the
balloon took on superheat whioh was lost_when the sun went down. ntis…
- p. 558 …the transmitter was not insulated, and there was no heat to be gained
.from the sun…
- p. 570 …Since the sun had set between the third and
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- p. 579 during the sunset descent (caused when the superheated helium lost the sun's
heating ei'i…
- p. 591 …that seen earlier with the balloon gas being warmed by the sun to acquire
a superheat…
- p. 666 …the changing buoyancy of the balloon as cloud
masses intermittently shielded it from the sun's…
- p. 736 …the
subst;q.uent descent, superheating of the balloons by
the nsmg sun would cause the…
- p. 739 …Flight termination was usually due to deteriora-
tion of the balloon caused by the sun.
In…
- p. 740 …the ambient tem-
perature after the sun had risen.
The automatic ballast valve operates. when the…
- p. 801 …April 14 Sun. Down to lab this am with Joe looking for G9A files. Jim Peoples…
- p. 802 …Discussed with Crane possibilities of getting sound through the ground part
of the ocean sound channel…
- p. 803 …Over to Jim and Rowes tonight and to Euzzards Bay bowling,
l'ay 5 Sun. L…
- p. 806 …Stayed at Amarillo -
at Clinton Hotel
Jan 19 Sun Left Amarillo about 1130 CST
IC.ent…
- p. 808 …Correlated between the ~ower and Dona
sites for se·reral sources. 'o!orked total travel times…
- p. 810 …April 6 Sun. Checked clocks. Cleaned out hanger and emptied trash out at East White Sands…
- p. 811 …April 20 Sun. Worked on plans for bombing runs and V2 monitoring.
April 21 Mon. Alamogordo…
- p. 812 …All equipment loaded on plane this pm.
~ay J-4 Sat, Sun. Left Alamogordo about 9…
- p. 815 …29 June (Sun) NYU personnel and some of Watson Lab men working today with equipment in…
- p. 816 …July 1a Sun. to cabins in Ohio just out of Springfield.
July 1 Mon. To cabins…
- p. 852 …4C.~~~ies• .tJi~J.tl~e ..•
a 'telemeteririg ·device to indicate· the rate of ballast flow…
- p. 861 …a sun-
set.
(3) By adding altitude control equipment, it is possible
to maintain the balloon…
the equation 2500 ft.3jlb.·mol = ae50b where 50 is the expression
for altitude in thousands of feet. Similarly, at 70,000 feet~
6450 =ae70b, and by solving to eliminate a, we find 2.58 = e Ob
or 20b = .95, and the constant b is equal to .0475. Thus, the
equation may be written:
(3)
y was originally defined as the molar volume, equal (for 98% helium)
to:
Balloon Volume x 24.4
Gross Load
K
=-w
K _ 08.o475Z
In turn, w-in thousands of feet.
W, the gross load.
, where z is the expression for altitude
From this relationehip, we may solve for
(4) w =
(5) In{~) = -.0475 i!
or:
(6) In W + In f = - .0 4 7 5 ~
Differentiating with respect to W:
(7) dz _ 21. 052 ft
crw-- w 1b where W is gross load in lb.
We see that the value of the constant a is unimportant here, and
the expression is independent of balloon volume, as long as it
does not var/ with time. Included is the assumption that over a
short period of ti~e buoyancy of lifti~gas does not change.
Thus, we have an expression for A, the altitude sensitivity, which
is valid between 40,000 and 105,000 feet. Similarly, it is possible
to evaluate altitude sensitivity for operation between 0 and 30,000
feet. A in this range is equal to 31,400 ft./lb.
VI
A plot of altitude sensit.ivity against load is shown on page 109
of the "Operations" section (Part II of this technical repo~.
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