SammyD
Well-Known Member
Hello everyone!
I ran into an issue that I'm hoping someone can help with. I've never experienced this before but at a recent launch in Bayboro, NC (Oct 14-15, 2017) a new scratch-built rocket traveled to an altitude and velocity that were different (substantially different in Flight 2) than the Open Rocket simulation in two successive flights. I'm using redundant altimeters that reported to within 1 foot of each other on altitude and within 1mph of each other on two different flights.
I have a new 4" Patriot that I scratch built made of BlueTube airframe and motor mount, 1/4" birch plywood fins and a LOC PNC-3.9 nosecone (more on this later). I'm not going to bore you with the OR design file as EVERYTHING has been checked and rechecked for accuracy!
Here is how the flights broke down from Stratologger CF altimeters:
Maiden Flight: CTI K-520, Simulation said 7545' and 696mph
Actual readings: Altimeter 1: 7600' and 661mph,
Altimeter 2: 7601 and 662mph. (Yes, I realize this speed is LOWER than the simulation, but see Flight 2)
Flight #2: CTI K-570, Simulation said 8514' and 765mph
Actual readings: Altimeter 1: 8916' and 890mph
Altimeter 2: 8917' and 890mph.
Here's is where I need help: Would a rounded nosecone like the one I'm using, a LOC PNC-3.9, cause the variations in altitude and velocity? It seems like I've read somewhere that a blunt nosecone like the one on the LOC 3.9 can/will cause air to move over the airframe more easily, thus giving me greater speed and altitude. It seems like I read that is the reason why the front end of so many jet aircraft have a big, bulbous nose on them: better aerodynamics...
Is this what is happening here? The ONLY variance in my design file and the actual rocket are the shape of the very tip of the nosecone. OR only allows a pointed nosecone (Ogive shape), but my nosecone has a bulbous end about the size of a quarter.
Had to drop a launch photo in here too
CTI K-520 in full burn at the end of the 1010 rail...:

I ran into an issue that I'm hoping someone can help with. I've never experienced this before but at a recent launch in Bayboro, NC (Oct 14-15, 2017) a new scratch-built rocket traveled to an altitude and velocity that were different (substantially different in Flight 2) than the Open Rocket simulation in two successive flights. I'm using redundant altimeters that reported to within 1 foot of each other on altitude and within 1mph of each other on two different flights.
I have a new 4" Patriot that I scratch built made of BlueTube airframe and motor mount, 1/4" birch plywood fins and a LOC PNC-3.9 nosecone (more on this later). I'm not going to bore you with the OR design file as EVERYTHING has been checked and rechecked for accuracy!
Here is how the flights broke down from Stratologger CF altimeters:
Maiden Flight: CTI K-520, Simulation said 7545' and 696mph
Actual readings: Altimeter 1: 7600' and 661mph,
Altimeter 2: 7601 and 662mph. (Yes, I realize this speed is LOWER than the simulation, but see Flight 2)
Flight #2: CTI K-570, Simulation said 8514' and 765mph
Actual readings: Altimeter 1: 8916' and 890mph
Altimeter 2: 8917' and 890mph.
Here's is where I need help: Would a rounded nosecone like the one I'm using, a LOC PNC-3.9, cause the variations in altitude and velocity? It seems like I've read somewhere that a blunt nosecone like the one on the LOC 3.9 can/will cause air to move over the airframe more easily, thus giving me greater speed and altitude. It seems like I read that is the reason why the front end of so many jet aircraft have a big, bulbous nose on them: better aerodynamics...
Is this what is happening here? The ONLY variance in my design file and the actual rocket are the shape of the very tip of the nosecone. OR only allows a pointed nosecone (Ogive shape), but my nosecone has a bulbous end about the size of a quarter.

Had to drop a launch photo in here too
CTI K-520 in full burn at the end of the 1010 rail...:

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