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Axial Tube Crush Tests

Last updated 07/04/2010

 

Carbon fiber tubes are PML's "Level 3 Series" These tubes nearly shut my testing machine down as they approached the limit of the load cell I was using.

This test consists of all 3" tubes. It directly compares the column strength of each tube. This is known as an axial load and is the primary load that an airframe sees. (Unless you step on your rocket, then see the bend test.)

The cardboard tubes show the added strength obtained by gluing in a coupler tube. It also shows the additional strength of a "stiffy" type coupler.

Some of the numbers on the website can be difficult to understand. To help you better understand, I have taken the test data from some tubes and compared them side by side b elow:



Tube Crush Specimen Results: Comparison of three tubes

Last updated 07/04/2010


Some of the numbers on the website can be difficult to understand. To help you better understand, I have taken some data from some of the tubes and compared them side by side. This is a discussion on the data shown.

Name Comment Blue Tube PML Phenolic Giant Leap Magnaframe
ID Actual measurement of the inside diameter of the tube as measured with a micrometer. 3.002" 3.000" 3.004"
OD Actual measurement of the outside of the tube as measured with a micrometer. 3.128" 3.132" 3.096"
Area ID subtracted from the OD, in square inches. This is the total surface area created by the wall thickness. 0.60662 in2 0.63572 in2 0.43757 in2
Modulus Stiffness - Load divided by extension. This is a measurement of how the tube starts to crush when a load is applied. 574.1 ksi 765.9 ksi 823.7 ksi
Peak Load Ultimate strength of the tube - This is the actual load placed on the tube. 3052.6 lbf 2573.6 lbf 2226.5 lbf
Peak Stress Peak load divided by the area (wall thickness) - This is the indicator of the actual strength of the material that the tube is made of. 5032.1 psi 4048.3 psi 5114.0 psi

Looking at the data above, you can make these statements:

Blue Tube PML Phenolic Giant Leap Magnaframe
Area Thickest Tube Thinnest Tube
Modulus Softest tube - can only be used to ˝ its peak load. Stiffest tube - can be used up to its peak load.
Peak Load Strongest because of its thickness. Lowest because of its thickness.
Peak Stress Weakest Material Strongest Material


Peak Load

This is the highest load that the tube withstood. Here we see that the Blue Tube withstood well over 3,000 pounds while the phenolic could only handle about 2,600 pounds. This may lead you to believe that the blue tube is stronger. While it is, that higher strength is not useable. If you look at the graphs, you will notice that the Blue Tube didn't even make it to 2,000 pounds before it began to deform and crush. You can see the line on the Blue Tube graph start to curve away from the straight line around 2,000 pounds. The phenolic made it all the way to 2,500 pounds before it began to deform. The line on this graph is straight all the way to failure. I do not have graphs for every test I've done on the site. But, there is another data point you can use that tells you what the graphs are telling you. It's called Modulus.

Modulus

Modulus, or "Modulus of Elasticity" is a measurement of a materials stiffness. Using the comparison above, you can see that the phenolic is much stiffer. This means that the material holds it's shape up to a higher load. There is a tradeoff in having a stiffer material. Although the phenolic can withstand more load because it is stiffer, it means that when it does "give", it cracks. This shows that, although actually weaker in use, the Blue Tube is tougher than phenolic. A good example the usefulness of a material's modulus is a rope. Since the modulus of a rope in compression is quite low, no matter how strong the rope is, pushing on a rope doesn't get you anywhere.

Peak Stress

On many of the tables, you will see the term "stress" On the above example you see peak stress. Stress is nothing more than (in this case) the "peak load" divided by the surface area. In the case of the tubes, "area" is derived from the wall thickness. The thicker the wall, the more load that the material can handle because of the increased surface area. An illustration is this: We know that carbon fiber tubing is stronger than phenolic tubing. A 3" diameter phenolic tubing with a 3/4" wall thickness could hold as much weight as a 3" diameter carbon fiber tube that only has a 1/16" wall thickness. They both have the same peak load, but the carbon fiber tube has a much greater peak stress value.

Using peak stress as the indicator of strength levels the playing field between samples. This shows the overall strength of the material and can help you chose a lighter tube for altitude records. Of course, using peak stress also makes it possible to compare the materials of the tubes, regardless of the tube diameter. This means that you can compare the LOC 5.5" cardboard tube against the USR 2.6" Glassine tubing.


3" Tubing
Specimen # Manufacturer Material/Notes Area
in^2
Peak Load
(lbf)
Peak Stress
(psi)
Modulus
BL-1 Always Ready Rocketry Blue Tube 0.60662 2974.1 4902.7 559.6
BL-2 0.60662 3211.1 5293.4 607.1
BL-3 0.60662 3052.6 5032.1 574.1
GLP-1 Giant Leap Plain Phenolic 0.53449 895.0 1674.5 427.4
GLP-2 0.60053 1299.9 2164.6 561.4
GLP-3 0.58360 1897.8 3251.9 681.4
GLD-1 Giant Leap Dynawind 0.72052 6531.0 9064.3 1184.1
GLD-2 0.68161 5956.5 8738.7 1248.0
GLD-3 0.71626 5545.1 7741.7 1118.7
GLM-1 Giant Leap Magnaframe 0.41688 2591.4 6216.1 901.0
GLM-2 0.45049 2084.8 4627.9 781.8
GLM-3 0.44534 2003.2 4498.1 788.4
GLMD-1 Giant Leap Dynawind Magnaframe 0.61686 5067.6 8215.2 1239.4
GLMD-2 0.66527 5945.3 8936.7 1115.1
GLMD-3 0.66527 5508.3 8279.8 1139.6
HM-1 Hawk Mountain Filament Wound Glass 0.59247 7935.708 13,450.0 Samples
HM-2 0.59247 9438.735 16,056.4 Test machine
HM-3 0.59247 9407.019 16,147.9  
1 LOC Plain Glassine 0.38202 711.8 1863.2 297.5
2 0.38202 757.7 1983.5 397.1
1 LOC With Regular Coupler 0.91509 1988.4 2172.9 439.5
2 0.91509 2252.7 2461.7 460.8
1 LOC With Stiffy Coupler 1.98776 3039.5 1529.1 300.7
2 1.98776 3319.8 1670.1 312.0
1 LOC Home Glassed Glassine 0.52787 1826.1 3459.4 702.6
2 0.52787 2100.6 3979.5 672.5
3 0.52787 2169.4 4109.7 696.7
PR-1 Performance Rocketry Filament Wound Glass 0.54324 12548.4 23099.2 2328.0
PR-2 0.50934 19256.1 37806.2 2980.8
PR-3 0.52349 17658.2 33731.2 2589.5
1 PML Quantum Tubing 0.49858 4332.6 8689.8 456.4
2 0.49858 4234.4 8492.7 456.6
3 0.49858 4484.3 8994.0 454.9
1 PML Plain Phenolic 0.63572 2573.6 4048.3 792.4
2 0.63572 2990.5 4704.2 802.5
After test 0.63572 3037.4 5054.6 800.0
1 PML Home Glassed Phenolic 0.66034 4544.0 6881.3 1079.2
2 0.66034 5388.4 8160.1 1057.2
3 0.66034 5137.7 7780.5 1084.4
1 PML Factory Glassed Phenolic 0.86369 6439.2 7455.5 1311.7
2 0.86369 7758.9 8983.4 1228.9
1 PML Level 3 Series Carbon Fiber 0.85870 25413.3 29595.1 4310.8
2 0.85870 27080.6 31536.7 4374.5
1 US Rockets USR Whitewall Tubing 0.78975 1067.3 1403.9 Picture
6 0.78975 1074.9 1397.1 Picture
Mean 0.78975 1152.4 1476.9 Picture

 

5.5" LOC/Precision Tubing
Specimen # ID" OD" Length" L/D Ratio Peak Load (lbf) Peak Stress (psi) Load at Yield (lbf) Stress at Yield (psi) Notes
1 5.370 5.52 12 2.174 2246.959 1751.402 ****** ****** Glassed
2 5.370 5.52 12 2.174 2290.050 1784.989 2008.750 1784.989 Glassed
3 5.370 5.52 12 2.174 2205.591 1719.158 2205.591 1719.158 Glassed
4 5.370 5.52 12 2.174 1312.738 1023.219 1312.738 1023.219 Un glassed
5 5.370 5.52 12 2.174 1221.385 952.013 ****** ****** Un glassed
6 5.370 5.52 12 2.174   1000.205     Un glassed


USR  2.6"Glassine Tubing
Specimen # ID" OD" Length" L/D Ratio Peak Load (lbf) Peak Stress (psi) Load at Yield (lbf) Stress at Yield (psi) Notes
1 2.639 2.690 24.0 8.922 550.883 2580.795 465.045 2178.659  
2 2.639 2.690 24.0 8.922 602.593 2823.046 486.074 2277.174  
3 2.639 2.690 24.0 8.922 500.208 2343.389 369.899 1732.917  
4 2.639 2.690 24.0 8.922 490.211 2296.554 490.211 2296.554  
Mean 2.639 2.690 24.0 8.922 535.974 2510.946 452.807 2121.326  
Std. Dev 0 0 0 0 51.749 242.435 56.359 264.034  


USR  2.25" Whitewall Tubing
Specimen # ID" OD" Length" L/D Ratio Peak Load (lbf) Peak Stress (psi) Load at Yield (lbf) Stress at Yield (psi) Notes
1 2.189 2.229 18.0 8.075 306.124 2205.576 299.919 2160.869  
2 2.189 2.229 18.0 8.075 313.364 2257.734 299.229 2155.901  
3 2.189 2.229 18.0 8.075 322.327 2322.311 306.124 2205.576  
Mean 2.189 2.229 18.0 8.075 313.938 2261.874 301.758 2174.1155 Picture
Std. Dev 0 0 0 0 8.116 58.478 3.797 27.359  


Blueprint Tubes
Specimen # ID" OD" Length" L/D Ratio Peak Load (lbf) Peak Stress (psi) Load at Yield (lbf) Stress at Yield (psi) Notes
1 3.158 3.300 24.0   1283.436 1781.959 1283.436  - Unknown Blue Print Tube


Shipping Tubes*

Specimen # ID" OD" Length" Peak Load (lbf) Peak Stress (psi) Load at Yield (lbf) Stress at Yield (psi) Notes
1 1.994 2.120 9.0 472.494 1160.569 - - Plain Ship Tube
2 1.994 2.120 9.0 476.744 1171.010 - - Plain Ship Tube
3 1.994 2.159 9.0 2865.135 5323.643 - - Plain Tube West Sys. Glassed
4 1.994 2.159 9.0 2681.320 4982.101 - - Plain Tube West Sys. Glassed
5 1.994 2.156 9.0 1801.274 3400.446 - - Plain Tube, Polyurethane Glassed
6 1.994 2.156 9.0 1851.036 3505.593 - - Plain Tube, Polyurethane Glassed
* The glassed tubes were two layers of 6 oz boat glass and vacuum bagged. The West Systems was the 105/206 and the polyester was Evercoat 105499 from Home Depot.

3" PML    3" PML   

Note that (in both cases) the PML failure was at the spiral grove. You guys that fill in your spirals with glue my have an added benefit you didn't even realize you had.

The USR whitewall tubes broke much differently than the PML. These tubes fan folded and never actually broke. The stress oscillated as this happened. 

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