Hello,
I recently certified L1, and am now having a lot of fun designing, in openrocket, options for the next rocket that I will build. I am looking at altitude-optimized, almost minimum diameter designs, so most are simulating at mach 1-1.3 max (with accelerations in the 15-20g range), using longer burning motor options. My question is, will standard small plastic nosecones, such as the LOC PNC-1.52 or apogee PNC 29, hold up to this velocity range?
Extensive googling and searching on this forum has revealed plenty of useful information about optimal shape and dimension, but most threads here seem to be about pushing mach 2 or 3. I'm hoping that a few of y'all will be able to share your experiences flying plastic nose cones in the transonic range. If anyone can point me to resources with these answers instead, that would also be greatly appreciated.
Thanks
-Jason
I recently certified L1, and am now having a lot of fun designing, in openrocket, options for the next rocket that I will build. I am looking at altitude-optimized, almost minimum diameter designs, so most are simulating at mach 1-1.3 max (with accelerations in the 15-20g range), using longer burning motor options. My question is, will standard small plastic nosecones, such as the LOC PNC-1.52 or apogee PNC 29, hold up to this velocity range?
Extensive googling and searching on this forum has revealed plenty of useful information about optimal shape and dimension, but most threads here seem to be about pushing mach 2 or 3. I'm hoping that a few of y'all will be able to share your experiences flying plastic nose cones in the transonic range. If anyone can point me to resources with these answers instead, that would also be greatly appreciated.
Thanks
-Jason