Does Heat Warp Quantum Tube?
Abstract
We've learned that poop pipe has a significant amount of thermal expansion when compared to other rocketry
materials. This is evidenced by the tests done on the “Effects of Temperature on
HPR Materials” page. Could this amount of thermal expansion be the culprit
in squirrelly rocket flights? I set up an experiment to see what happens if a
rocket is left in the sun during a launch. One side of the rocket gets full
sun, while the other side is left in shade.
Very few rockets in our hobby don't have at least some spin on the way up. As a bent or curved rocket spins in flight it corkscrews.
Take Eric Salerno’s PML Endeavor. This rocket has been known to
fly “squirrelly” on hot sunny days. On at least two occasions, the trajectory
of the rocket has exhibited a corkscrew pattern. On one occasion, a bend in the
rocket could actually be seen while sitting on the pad. It was hypothesized
that when sitting in the sun, one side of the rocket heats up, and the shade
side stays relatively cool. This would cause the tube to expand on the hot side
and warp the airframe.
Postulate
Does Quantum Tubing warp in the sun, causing a temporary warp in the airframe?
Investigation
Test Outline
A rocket would be place on a fixture. It would be rotated
and measured for any deviation from straightness using a calibrated dial
indicator. External influential factors would be measured while conducting the
test such as rocket temperature on both the sun side and shade side, along with
several ambient weather conditions. All measurements would be taken prior to
conducting the test in the sun to establish a baseline.
Fixturing
The fixture was made with a 1 x 6 pine board. One inch holes
were drilled to accommodate a V-block on each end. The V-blocks were placed 18”
apart. This distance was chosen because there was a coupler and a PML CPR 3000 in the center. I believe that the coupler
would stiffen the center 4” of the tube and reduce the effective tube length to
14”, or 1.16 feet. A stop was secured to the plywood to
ensure that the dial indicator would always trace the same circumference
location.
The fixture assembly was placed on a table and was checked
for stability. A dial indicator was secured to a magnetic base. The magnetic
base was secured to steel for stability.
The whole assembly was tested for stability and
repeatability. The forward section of a maroon painted PML Endeavor was placed in
the V-blocks and butted up against the stop before exposure to the sun. This is
the actual rocket mentioned in the abstract of this paper. A mark was placed on
the tube to ensure that the same location was always up after rotational
measurement.
At the start of the test
Equipment Used
| Rocket: | PML Endeavor |
| Thermocouple: | Omega Type K PN SP-RL-K-6 SN# PL093007 (New) |
| Thermometer: | Omega 450 AKT Type K SN# 94050175 |
| Dial indicator: | Federal “Miracle Movement” C81– 0.290” max travel |
| Base: | NOGA magnetic base |
| Ambient Sensor: | Fisher Scientific “Thermo-Hygro” NIST Traceable #240180578 |
First Test Conducted
The skies were partly cloudy with a light breeze from the
WSW. The ambient temp ranged from 73°F to 75°F. The relative humidity started
at 63% and steadily fell to 50%. The clouds caused problems during testing as
the sun kept going behind the clouds and the surface of the rocket kept cooling
off. I thought of scrapping the test for the day until I realized that this
would eliminate the possibility of some other influence causing the tube
bending. It quickly became apparent: more sun, more bend, less sun, less bend.
The test was concluded when the clouds became increasingly abundant.
During the test
Measuring the temperature
The results were clear: the tube bent upward when heated by the sun.

Figure 1 Graph showing plotted data
Second Test Conducted
Since the weather conditions were variable, a second test
was conducted. The skies were clear with a light breeze from the SW. The
ambient temperature remained constant at 75°. The relative humidity ranged from 62% to
55%. In the interest of uniformity, the test was conducted at the same time of
day.

Figure 2 Graph showing plotted data
Discussion
When most any material is heated, it expands. This is true
for Quantum Tubing. As demonstrated in the “Effects of Temperature on
HPR Materials” test, Quantum Tubing expands and contracts greater than
other rocket building materials such as wood or fiberglass. That test
demonstrated this, and why pistons get stuck when it is cold outside.
As the sun heats up the tubing, it expands. Since the ½ of
the tube is in the shade, the sunlit side gets hotter than the shaded side.
While the material expands on the sun heated side, the shaded side stays
relatively constant. This causes the tube to bend.

Figure 3 Illustrating one side heated resulting in bending
The graphs clearly show that as the surface of the rocket
heats up, the tube becomes more bent. The greater the temperature, the greater
the bend.
Looking at the graphs, we also notice that the greatest
difference in “Tube Temp” to “Deflection” correlates with the difference in
“Sun Side” to “Bottom Side”. This shows that the greater the temperature
differential, the greater the bend. This is most evident in the 12:04 PM EST
data points on the Aug 15 graph, Figure 1.
Since we measured the deflection at ½ of the distance
between the V-blocks, we can assume that the total deflection, as measured from
one end to the other is 2 times the deflection. With an effective test distance
of 14”, we can formulate the following:
Def x 2 / 1.16 = Total Deflection per foot
The greatest deflection was 0.030”. Thus:
0.030 x 2 / 1.16 = 0.052” per foot
This means that a 6 foot tall rocket can bend at least 5/16”.
On the second day of testing, the temperature of the nose
cone was measured. When the test area read 126.5°F, the nosecone was 142.8°F.
Conclusions
1. The
evidence shows that when one side of a rocket made from Quantum Tubing, the sun
side expands more than the shaded side.
2. The
evidence suggests that for every ~52°F differential heating on a Quantum Tube,
a 4” diameter rocket will bend ~0.052” per
foot.
3. To
reduce the amount of “heat bending” and for straighter flights, keep your
rocket in the shade, and paint it a light color.
Appendix A
Raw Data collected:
|
First Test Quantum Tube Test – 15 Aug., 2008
|
|
Time (EST)
|
Humidity (%)
|
Ambient Temp (ºF)
|
Sun Side Temp (ºF)
|
Shade Side Temp (ºF)
|
Deflection (Inches)
|
|
11:51
|
63
|
73
|
72.6
|
72.6
|
0.000
|
|
11:54
|
57
|
73
|
101.4
|
77.0
|
0.014
|
|
11:56
|
53
|
73
|
90.2
|
77.0
|
0.008
|
|
12:01
|
55
|
73
|
104.3
|
78.3
|
0.019
|
|
12:04
|
55
|
73
|
98.1
|
72.8
|
0.009
|
|
12:11
|
53
|
73
|
115.8
|
82.8
|
0.021
|
|
12:23
|
53
|
75
|
116.9
|
78.9
|
0.024
|
|
12:31
|
51
|
75
|
134.8
|
82.2
|
0.030
|
|
12:44
|
50
|
75
|
125.2
|
83.6
|
0.026
|
|
12:51
|
50
|
73
|
97.4
|
77.0
|
0.007
|
|
Second Test Quantum Tube Test – 16 Aug., 2008
|
|
Time (EST)
|
Humidity (%)
|
Ambient Temp (ºF)
|
Sun Side Temp (ºF)
|
Shade Side Temp (ºF)
|
Deflection (Inches)
|
|
11:55
|
62
|
75
|
73.4
|
73.0
|
0.000
|
|
11:58
|
62
|
75
|
104.6
|
77.5
|
0.013
|
|
12:01
|
60
|
75
|
116.3
|
79.5
|
0.0205
|
|
12:05
|
58
|
75
|
123.5
|
78.6
|
0.024
|
|
12:12
|
59
|
75
|
127.7
|
83.4
|
0.0265
|
|
12:20
|
58
|
75
|
124.0
|
82.3
|
0.026
|
|
12:28
|
55
|
75
|
133.4
|
87.2
|
0.027
|
|
12:37
|
57
|
75
|
137.2
|
82.0
|
0.026
|
|
12:45
|
57
|
75
|
126.5
|
78.9
|
0.025
|
|
12:59
|
55
|
75
|
131.8
|
80.0
|
0.028
|
|