Yes but I need to do some errands this evening but I'll do a basic outline
when I return, emphasis on 'basic'.
K
On Fri, Apr 9, 2021 at 7:39 PM Tyler Adkison <tyler.adkison@xxxxxxxxx>
wrote:
Any advice on laying up the chevron pattern? I've never done a composite
layup in that style before.
Thanks.
On Fri, Apr 9, 2021 at 6:30 PM Brian Feeney <alaiadesign@xxxxxxxxx> wrote:
Is that a LOX / Kerosene engine at the 40KLbF rating?
What chamber pressure is the TCA at for the 40KLbF rating?
Thank you!
Brian
On Fri, Apr 9, 2021 at 9:14 PM roxanna Mason <rocketmaster.ken@xxxxxxxxx>
wrote:
Tyler, drawing of 40KLbF Ablative TCA, note chevron pattern for maximum
resistance to high velocity high temp gas erosion
Thanks,
Ken
On Fri, Apr 9, 2021 at 1:41 PM Tyler Adkison <tyler.adkison@xxxxxxxxx>
wrote:
I, for one, would be interested in these drawings as well. If you could
link them here or send them to me as well, it would be much appreciated.
Thanks,
Tyler
On Fri, Apr 9, 2021 at 11:25 AM roxanna Mason <
rocketmaster.ken@xxxxxxxxx> wrote:
Hello Jon. I personally contributed to the manufacture of a number of
ablative TCA's, 1,1.5, 5 and 20KLbF, the former is an online video of it
under hot testing.
I have some drawings that I could scan and email though knowledge of
construction details is something else.
Thank you and good luck,
Ken
On Fri, Apr 9, 2021 at 5:46 AM Jonathan Adams <jonadams2002@xxxxxxxxx>
wrote:
Hello everyone,
I'm getting to the construction stage of a 4.5kN ablative liquid
propellant engine, and I was wondering if anyone had any good resources
for
composite layup for the ablative wall. Possibly even resources specific
to
composite layup for small rocket engines.
I haven't been able to find many good resources out there for how to
do this, and I wanted to know if anyone could point me in the right
direction for how to go about this. Even personal experience for how to
do
this right (and cost-effectively!) would be greatly appreciated.
Thanks,
Jon.
