[AR] Re: Solid rocket insulation, yet again

  • From: Henry Vanderbilt <hvanderbilt@xxxxxxxxxxxxxx>
  • To: arocket@xxxxxxxxxxxxx
  • Date: Tue, 24 Apr 2018 11:40:20 -0700

Stop me if this has already been tried and found wanting... But I gather an EPDM liner is generally superior but a pain to install, especially at smaller diameters?

I see that EPDM is available as tubing. Perhaps start with a piece of EPDM tubing of slightly smaller diameter and slightly greater length than the metal tube to be lined. Seal both EPDM tube ends, with a shrader valve (or similar) installed in one. Coat the EPDM tube exterior, the metal tube interior, or both with a suitable adhesive - it'd need to be relatively slippery long enough for the next step. (Possibly add solvent, which might also help the EPDM expand to the metal tube diameter without residual tension?) Then pull the EPDM tubing through the metal tube. Pressurize the EPDM tubing to expand it firmly against the metal tubing. Maintain that pressure till adhesive sets, trim the ends, done.

Assuming there aren't already known show-stoppers, I expect it would still take a certain amount of cut-and-try on someone's part to get this working reproducibly. But given the current procedures I've seen described here, it still might end up as an overall simplification.

Henry

On 4/24/2018 10:27 AM, William Claybaugh wrote:

Ed:

Interesting.

How do you know that there are no voids on the liner surface?  I’m thinking that surface grinding the OD of the liner (which the manufacturer does anyway) should get a void free surface.  The issue then becomes—as Korey observed—the out of roundness of the tube.

In theory, a limited amount of flexibility should allow the phenolic to conform to the tube. For these 9” OD tubes (worked to + / - 0.010 on the ID) it appears that the 8.480” nominal OD phenolic is a very tight fit (I just started fitting the phenolic this morning).

I’ve seen folks use grease but always thought it was for getting the phenolic in and out; it seems unlikely it would provide enough support to prevent cracking of the liner.

I like the parchment paper idea; I will give it a try if there proves to be any room.

Bill

On Tue, Apr 24, 2018 at 11:07 AM Edward Wranosky <edwardcw@xxxxxxxxx <mailto:edwardcw@xxxxxxxxx>> wrote:

    In HPR rocket motors some people slather an excess of grease on the
    outside of the liner to fill the gap (if present) between the liner
    and the casing.  I prefer having to sand down the liner and using
    some elbow grease to get it into the casing over having a gap. I got
    tired of small diameter liners cracking (1.5"-3" diameter motors) so
    I typically build the liner up with epoxy, sand down and then apply
    single wrap of parchement paper so it doesn't stick to the casing.

    Edward

    On Tue, Apr 24, 2018 at 10:58 AM, William Claybaugh
    <wclaybaugh2@xxxxxxxxx <mailto:wclaybaugh2@xxxxxxxxx>> wrote:

        Troy:

        I agree that getting (cool) gas to the back of a phenolic liner
        is crucial.  I burnt through three very thin (0.050”) walled
        2.5” diameter motors until I worked out a labyrinth gas path
        that cooled the gas against the bulkhead mass before letting it
        pressurize behind the phenolic.

        On the whole, I’m not a big fan of phenolic for insulation
        exactly because it requires gas on the motor tube wall.  But for
        very small diameters, it is easier than laying in epdm sheet....

        Bill

        On Mon, Apr 23, 2018 at 10:35 PM Troy Prideaux
        <troy@xxxxxxxxxxxxxxxxxxxxx <mailto:troy@xxxxxxxxxxxxxxxxxxxxx>>
        wrote:

            To me, your methodology – if enough scrutiny and care is
            taken – is sound enough. There should be enough stretch (I
            know phenolic isn’t exactly the most flexible of materials)
            to accommodate that level of clearance over a large diameter
            although I’ve never used a ¼”(ish) thick liner before so…____

            __ __

            In smaller motors, this issue is problematic for designs
            that completely seal the liner with o-rings or whatever
            sealing so that no chamber gas is ever exposed to the
            outside of the liner. Designs that allow the gasses to pass
            to the outside of the liner (where the sealing is done
            against the motor casing) tend to not be so susceptible to
            liner cracking. Not sure how common or sound that approach
            would be for larger motors.____

            __ __

            Troy____

            __ __

            *From:*arocket-bounce@xxxxxxxxxxxxx
            <mailto:arocket-bounce@xxxxxxxxxxxxx>
            [mailto:arocket-bounce@xxxxxxxxxxxxx
            <mailto:arocket-bounce@xxxxxxxxxxxxx>] *On Behalf Of
            *William Claybaugh
            *Sent:* Tuesday, 24 April 2018 1:52 PM
            *To:* arocket@xxxxxxxxxxxxx <mailto:arocket@xxxxxxxxxxxxx>
            *Subject:* [AR] Solid rocket insulation, yet again____

            __ __

            I had a nice visit w/ Kory Kline over the weekend. Whilst
            looking over my two-stage hardware he noted that because
            extruded aluminum tubes are always out of round, he and
            found that phenolic liners failed by cracking into the
            inevitable gap upon ignition.____

            __ __

            His solution to this issue was to spin cast a liner of htpb
            mixed w/ carbon black and then cast a monolithic grain into
            that lined tube.  This seems to me clever; he suggested that
            it does work.____

            __ __

            My own approach has been to straighten the tube until the
            bulkhead will pass through it, end to end. This leaves a
            maximum of 0.010” of clearance on the phenolic liner (which
            has the same OD as the bulkhead); that has not proven to be
            a problem in a total of eight firings at 9” diameter.____

            __ __

            Are there other solutions to the extruded tube out of
            roundness issue?____

            __ __

            Bill____

            __ __

            __ __



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