And grain configuration. I am certain that moonburners and C slots have offset
thrust, there's only so much the convergent section of the nozzle can do.
On June 17, 2015 4:44:03 PM PDT, R Dierking <applerocketry@xxxxxxxxxxx> wrote:
So, what do you think? Malformed nozzles, chamber pressure too high,
exhaust gases thrust vector rocket...
Sent from my iPhone
On Jun 17, 2015, at 4:24 PM, "Kurt Gugisberg" <kurtgug@xxxxxxxxx>wrote:
left the pad. I had to leave my casing with David because it had a
From the video, I could see that my Punisher also veered off after it
heat bulge in the end near the forward seal. So it was probably close
to catoing too.
behavior we saw: misaligned thrust vectoring, rail button placement,
Looks like we have a cast of characters that might lead to to
low level of stability with high thrust motor. The only thing it might
not be is rail whip.
<applerocketry@xxxxxxxxxxx> wrote:
Kurt
On Wed, Jun 17, 2015 at 1:02 PM, R Dierking
this misalignment problem.I’m sure we can come up with things to investigate and even reduce
the same K1440 engine and leave it up to each flyer if they are going
Who’s interested in a Punisher 2 mass launch? I think we should use
to modify the rail buttons, pad, whatever else. We have lots of time
to collect details on each project.
used to test for misalignments?
Chris, would it be possible to post some details of the AC stand
max thrust is achieved would help?
Do you think that creating a way to hold the rocket on the pad until
wouldn’t he be one of the best people to advise on something like this?
I’m wondering why David Reese has not joined this discussion because
launches would be cool and we probably wouldn’t need the contribution
Again, I think building a large launch pad/test stand for ROC
of many people to do it. We could use the pad at Black Rock for XPRS
or BALLS. Again, I’m offering to buy the trailer for the project.
Richard Dierking
