Fin Design Overview
The shape of the fins for Hermes 2 was almost identical to Hermes 1, except for the addition of a phenolic leading edge with a taper of 15 degrees. Phenolic was used as the leading edge because it is an ablative, which forms a char layer as the leading edge heats up from the airflow of the rocket, and burns away, getting rid of some of the heat generated. This is to protect the rest of the fin from the heating that we expect at supersonic speeds (Mach 3-4). The fin core was made out of 1/8" G10 (garolite sheet), and the phenolic leading edge was cut from a sheet of 1/4" phenolic which was later tapered and milled down 0.020" on each side.
The G10 is referred to as the "fin core" because it will eventually be covered with layers of carbon fiber during the fin can layup process to increase strength. G10 was selected because it is relatively inexpensive, and we think it is strong enough for our purposes (Hermes 1 also used G10 as the fin core material and the fins were still intact after the flight), but in the future, more analysis should be done to find stronger materials that are suitable for higher speeds.
Test Fin Can Fins
Below is a picture of the fins used for the test fin can layup. These dimensions were obtained from our OpenRocket sim, but were not the updated shape of the fins. This was acceptable for the test fin can layup, but for the flight candidate layup the shape was different.
Flight Candidate Fin Design Process
Talk about design of phenolic slot (0.3" deep, 1/16" thick)
[INSERT IMAGE]
Flight Candidate Fin Manufacturing Process
The fins for the flight fin can were made out of a 1/8" sheet of G10, with a phenolic leading edge made from 1/4" phenolic sheet. The fin core is G10 and had a tab cut into its leading edge, and the phenolic piece (with a slot cut into it) fits over the leading edge of the G10 fin. Below were the steps used to manufacture and assemble the fins. All of the machining was done in Gelb (Todd's shop in the basement of the Unified Lounge).
Materials Required:
Part One: Waterjet G10 Fin Core (~2 hours)
*Delamination is when the layers of your composite start coming apart. This can happen if the waterjet is cutting too quickly/strongly, and especially if your composite sheet is thin (1/8" is considered pretty thin).
Part Two: Waterjet Phenolic (~2 hours)
Part Three: Cut 1/16" G10 Tab on Mill (~4 hours)
In this step, you're cutting the 1/16" (0.0625 in) tab on the G10, which will be epoxied into the phenolic slot. In order to leave room for the epoxy, you want to make the tab thinner than 1/16", so we chose a tab thickness of 0.058".
Fin 1 | Fin 2 | Fin 3 | Fin 4 | Extra Fin (1) | Extra Fin (2) | |
---|---|---|---|---|---|---|
Average thickness x (in) | ||||||
Y-value of first cut = (x - tab thickness*)/2 | ||||||
Y-value of second cut = Diameter of cutting tool + x - tab thickness* |
*Tab thickness = 0.058"
After we cut the G10 tabs, we noticed that certain areas were thicker than others, particularly in the middle of the part. This could be because we only used one pass on the mill when cutting either side, and since the tab is so thin, it probably moved back and forth slightly as the mill was passing over it. We used 60 grit sandpaper to sand the thicker areas afterwards, but in the future, it would be more ideal to use several passes, and to consider decreasing the tab thickness so that it fits more easily into the phenolic slot.
Part Four: Cut Phenolic Slot
*After some brief research, we found that machine oil and ethanol doesn't have an adverse effect on phenolic. However, this could be incorrect, so more research should be done to determine whether a better procedure for cutting the slot exists, and whether either of these materials decreases the strength of the phenolic somehow.
Part Five: Cut Phenolic Taper
Part Six: Mill Down Phenolic
Use machining tape to stick phenolic down, edge at edge of clamp thing
Take off 0.020" inch, adjust mill when you turn it over to take off additional 0.020"
Part Seven: Assemble Fins
Lessons Learned:
Software
I used Solidworks to model the fins that were used on Hermes. Solidworks will also be used to design the phenolic - G10 interface and assemblies.
Are there any limitations of this software? Make suggestions for how you could design the part better if we had a different program/more time
Hardware/Manufacturing
Once you know the requirements of the part, list the materials you need to build it
Make a rough draft of the steps required to build the part
Laser Cutting the Part:
Create a DXF file of the part
Using illustrator, place the drawing on to an artboard the size of the wood
Adjust the settings on the laser cutter to appropriate settings for material
Cut!
Water Jet:
Transfer DXF file onto USB stick and onto waterjet computer
Place the material on the waterjet, set the origin, and make sure the drawing is within the limits of your material and the jet.
Cut each fin, making sure to stop in between and remove finished fins
Delamination can be avoided by:
Using the “Low Pressure” and “Brittle Material” setting on the waterjet
Lead into the bottom corner of the trailing edge instead of the top corner of the leading edge
Lead in before cutting (the waterjet turns on as it’s coming in to cut instead of starting right on the part)