11bravo
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The other thread going has gotten me thinkkng and lead to some questions.
1. If a person got a coupler for 38mm tubes to use as a mandrel for an all CF frame, would they need to add a couple of wraps of something to add just a smidge to the diameter to give room for the motor to actually slide into the airframe?
2. (I know this could vary widely, but...) what kind of wall thickness is common per layer of CF?
3. On a minumum diameter rocket, what do you do about the rear closure of the motor that extends beyond the OD of the BT?
Attached is a file that I came up with tinkering around.
The BT "ring" at the rear is to simulate that knurled rear closure on AT motors.
Of course, I simmed it using a Cessaroni.
Depending on whether I kept it at minimum weight (mass) for speed or optimal weight for altitude, I think I got good numbers either way.
It'd probably shred, but that's why one does it in RS; costs less money.
Answers to the questions or ideas on the rocket would are sought,
Greg
1. If a person got a coupler for 38mm tubes to use as a mandrel for an all CF frame, would they need to add a couple of wraps of something to add just a smidge to the diameter to give room for the motor to actually slide into the airframe?
2. (I know this could vary widely, but...) what kind of wall thickness is common per layer of CF?
3. On a minumum diameter rocket, what do you do about the rear closure of the motor that extends beyond the OD of the BT?
Attached is a file that I came up with tinkering around.
The BT "ring" at the rear is to simulate that knurled rear closure on AT motors.
Of course, I simmed it using a Cessaroni.
Depending on whether I kept it at minimum weight (mass) for speed or optimal weight for altitude, I think I got good numbers either way.
It'd probably shred, but that's why one does it in RS; costs less money.
Answers to the questions or ideas on the rocket would are sought,
Greg