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To match conditions similar to those expected from the high speed flight, a blowtorch will be used to heat small samples while a thermocouple will monitor the surface temperature of the materials. After the test we will also be measuring the samples to estimate the ablation. A stand has been built to hold the propane blowtorch at a specific distance from the samples and a remote trigger mechanism allows operators to be a safe distance from the blowtorch and sample.

 The tests will be performed in a secure environment (blast chamber) and the operators will wear respirators during the tests. This document from Apogee Components was used as inspiration for this test procedure. Apogee Newsletter

Materials Used:

  • Fiberglass
  • West Systems 105 epoxy (resin + hardener)
  • Phenolic microballoons
  • POR 15 High-temp Heat Resistant Paint
  • 400-grit sandpaper
  • Dremel 
  • Worthington propane blowtorch (14.1oz)
  • Arduino Uno
  • Thermocouple Amplifier MAX31855 breakout board (MAX6675 upgrade): https://www.adafruit.com/product/269

  • K-type thermocouple: https://www.adafruit.com/product/270

  • Jumper wires

  • Breadboard
  • Test stand

Below is the matrix for samples used in this thermal test.

 5-Layer Fiberglass10-Layer Fiberglass
Control (West Systems epoxy)  
West Systems + Phenolic microballoons  
West Systems + Cork microballoons  
West Systems + High temperature paint  
West Systems + Cotronics 4700  

Sample Preparation:

  1. Used West Systems epoxy to make 4 of 8" x 8" sheets of fiberglass (2 x 5 layers, 2 x 10 layers)
  2. Sanded with a Dremel, then with 400-grit sandpaper. Make sure to sand the shiny side as well
  3. Mark and cut into 1.5" x 1.5" squares.
  4. Recorded dry mass of each sample
  5. Took three measurements of thickness on three different sides, and calculated/recorded average thickness
  6. Wearing respirators, mixed 50 g. West Systems resin + 9 g West Systems hardener
  7. Mixed in phenolic microballoons until a consistency slightly thinner than peanut butter (like melted ice cream) was reached
  8. Applied phenolic mixture using popsicle sticks and left to cure for 36 hours
  9. Recorded average thickness of samples with phenolic coating
  10. Sanded with 400-grit sandpaper then recorded mass (and wiped with acetone)
  11. Applied high-temp paint to fiberglass samples (series 6,7) and fiberglass + phenolic samples (series 8,9)

Below is the test matrix for the parameters measured during this test. (Fill later with results).

 Fiberglass- CONTROLFiberglass + Phenolic MicroballoonsFiberglass + High-temp Fiberglass + Microballoons + PaintPhenolic
 5-Layer10-Layer5-Layer10-Layer5-Layer10-Layer5-Layer10-Layer   
 2-1'2-2'2-3'3-1'3-2'3-3'4-1'4-2'4-3'5-1'5-2'5-3'6-1'6-2'6-3'7-1'7-2'7-3'8-1'8-2'8-3'9-1'9-2'9-3'1-1'1-2'1-3'
Initial dry mass (no hole) - oz0.1350.1300.1500.2900.2950.2800.1400.150oz0.1600.3050.3000.3050.1500.1300.1350.2950.2800.3050.1400.1400.1400.2700.2700.2850.7850.7800.780
Initial dry average thickness - mm1.0166671.011.0433332.0533331.9966671.950.9933330.9633331.0833332.1266672.132.0466671.0933330.9366670.911.9366671.841.8866670.8466670.840.8033331.751.7533331.756.26.1533336.13
Thickness 11.030.981.032.082.02211.011.062.262.052.011.070.920.881.921.831.850.790.840.841.81.81.786.186.166.14
Thickness 20.9711.062.022.021.9410.941.072.082.162.061.160.920.911.941.851.890.860.850.811.751.741.746.216.156.12
Thickness 31.051.051.042.061.951.910.980.941.122.042.182.071.050.970.941.951.841.920.890.830.761.71.721.736.216.156.13
Initial wet mass (no hole) - oz                           
                            

Test Stand

<insert pics> 

Setting up thermocouples

 

Samples

Test Procedure:

Testing in blast chamber

Heat for 12 seconds

 

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