Overview:

To match conditions similar to those expected from the high speed flight, a propane blowtorch will be used to heat small samples of different materials with different ablative coatings (see test matrix below) while a thermocouple will monitor the surface temperature of the materials. The mass and thickness of the samples will be measured before and after the test to determine the effectiveness of the ablative coating used. A test stand has been built to hold the propane blowtorch at a specific distance from the samples (which can be adjusted as necessary). 

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:

Safety Notes:

Below is the matrix for samples used in this thermal test. All samples measured ~2" x 2" (with thickness depending on the sample), and there are three samples for each combination (for three trials). Each sample is labeled by "series" (1-9) with a hyphen, followed by the number of the trial. (so the nomenclature is series-trial number, for example: 4-2)

1/4" phenolic sheetSeries 1
 5-Layer Fiberglass10-Layer Fiberglass
Control (West Systems epoxy)Series 2Series 3
West Systems + Phenolic microballoonsSeries 4Series 5
West Systems + High temperature paintSeries 6Series 7
West Systems + Microballoons + paintSeries 8Series 9

Fiberglass 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), making sure to put Mylar beneath to keep the samples from sticking. 
  2. Let the samples cure for at least 24 hours. 
  3. Sanded with a Dremel, then with 400-grit sandpaper. Make sure to sand the shiny side as well. 
  4. Mark and cut into 1.5" x 1.5" squares using a Dremel
  5. Recorded dry mass of each sample (series 1-9)
  6. Took three measurements of thickness on three different sides of the sample, and used this to calculate/record average thickness (series 1-9)
  7. Wearing respirators, mixed 50 g. West Systems resin + 9 g West Systems hardener (100:18 ratio for West Systems, but this depends on the epoxy you choose to use)
  8. Mixed in phenolic microballoons using a popsicle stick until a consistency slightly thinner than peanut butter (like melted ice cream) was reached.
  9. Applied an even but thin layer of phenolic mixture to samples (series 4, 5, 8, 9) using popsicle sticks
  10. Let samples cure for 36 hours.
  11. Wipe samples with acetone to remove any dust or debris.
  12. Recorded average thickness of samples with phenolic coating (series 4, 5, 8, 9)
  13. Sanded with 400-grit sandpaper then recorded mass (and wiped with acetone)
  14. Applied high-temp paint to fiberglass samples (series 6,7) and fiberglass + phenolic samples (series 8,9)
  15. Let paint dry for at least 24 hours (depending on what paint you use)
  16. Wipe samples with acetone to remove any dust or debris.
  17. Record mass of each sample (series 6, 7, 8, 9)
  18. Record average thickness of each sample (series 6, 7, 8, 9)

Test Procedure:

  1. Testing in blast chamber
  2. Heat for approximately 12 seconds

Below are some pictures of the test stand, thermocouple used, Serial Monitor showing that the thermocouple works, and the fiberglass samples used (before they were cut and ablative coating was added)

Test #1: 

The first thermal test we conducted was on a single 5-layer control sample of fiberglass (using West Systems epoxy). The purpose of this test was simply to see what improvements needed to be made for the next test, during which more samples will be tested. Below are photos of the sample after the test, as well as a graph of temperature vs. time. 

Test Details:

Observations:

Improvements for Next Time:


Test #2: 


Final Results:

Below is a table showing the results of the thermal tests. Consult the test matrix above to see what each "series" corresponds to (for example, "Series 1" means 1/4" phenolic sheet). All samples measured 2" x 2" in area. For a more detailed spreadsheet, consult the attached Excel spreadsheet. (ATTACH SPREADSHEET) In the table below, since some samples have multiple layers of ablative coating, a key is used to denote the mass/thickness of each layer, followed by the total mass/thickness.

F = fiberglass

P = phenolic sheet

PM = phenolic microballoons

H = high-temperature paint

*Mass of sample measured after hole drilled (to attach sample to test stand) and after all ablative coatings have been added, which is why there is a discrepancy between the total mass and the sum of the masses of each layer. In some cases, the mass measures zero for the high-temperature paint because the scale was not accurate enough and the layer was thin.

 Series 1Series 2Series 3Series 4Series 5Series 6Series 7Series 8Series 9
Trial123123123123123123123123123
Initial mass* [oz]P: 0.780P: 0.780P: 0.780F: 0.135F: 0.135F: 0.145F: 0.290F: 0.295F: 0.280

F: 0.140

PM: 0.050

Total: 0.200

F: 0.150

PM: 0.065

Total: 0.220

F: 0.160

PM: 0.060

Total: 0.220

F: 0.305

PM: 0.075

Total: 0.365

F: 0.300

PM: 0.055

Total: 0.355

F: 0.305

PM: 0.050

Total: 0.355

F: 0.150

H: 0.000

Total: 0.145

F: 0.130

H: 0.005

Total: 0.135

F: 0.135

H: 0.000

Total: 0.140

F: 0.295

H: 0.000

Total: 0.290

F: 0.280

H: 0.000

Total: 0.280

F: 0.305

H: 0.000

Total: 0.305

F: 0.140

PM: 0.04

H: 0.000

Total: 0.180

F: 0.140

PM: 0.045

H: 0.000

Total: 0.185

F: 0.140

PM: 0.045

H: 0.000

Total: 0.185

F: 0.270

PM: 0.035

H: 0.000

Total: 0.305

F: 0.270

PM: 0.035

H: 0.000

Total: 0.310

F: 0.285

PM: 0.035

H: 0.005

Total: 0.320

Initial average thickness [mm]P: 6.20P: 6.15P: 6.13F: 1.02F: 1.01F: 1.04F: 2.05F: 2.00F: 1.95

F: 0.99

PM: 0.7

Total: 1.69

F: 0.96

PM: 0.76

Total: 1.72

F: 1.08

PM: 0.62

Total: 1.70

F: 2.13

PM: 0.70

Total: 2.83

F: 2.13

PM: 0.54

Total: 2.67

F: 2.05

PM: 0.56

Total: 2.61

F: 1.09

H: 0.04

Total: 1.13

F: 0.94

H: 0.08

 Total: 1.02

F: 0.91

H: 0.06

Total: 0.97

F: 1.94

H: 0.10

Total: 2.03

F: 1.84

H: 0.18

Total: 2.02

F: 1.89

H: 0.19

Total: 2.08

F: 0.85

PM: 0.42

H: 0.28

Total: 1.55

F: 0.84

PM: 0.59

H: 0.31

Total: 1.75

F: 0.80

PM: 0.53

H: 0.35

Total: 1.68

F: 1.75

PM: 0.55

H: 0.25

Total: 2.55

F: 1.75

PM: 0.53

H: 0.33

Total: 2.61

F: 1.75

PM: 0.52

H: 0.35

Total: 2.62

Final mass [oz]0.785  0.115  0.285                    
Final average thickness [mm]                           

Useful links:

https://tfaws.nasa.gov/TFAWS12/Proceedings/Aerothermodynamics%20Course.pdf