Mostly Harmless
Member
Hi all;
Trying my hand at scratch building a plane of my own design of the sort seen here:
http://www.flitetest.com/articles/300-g-plane-design-80-mins-with-1600-mah-battery
Along with learning how to minimize weight by construction techniques, I need to learn to use new materials -- specifically the carbon fiber tubes and rods.
I'm trying to gauge what size tube would be needed for a ~30" tail boom for a 60" wingspan aircraft -- minimizing weight, while keeping it strong enough to survive flight (and not flex mid-flight). Looking at all the various sources on line, I can't get a good feel for what size and wall thickness will meet my needs.
Can anyone offer any suggestions or guidance on selecting the right size for a tail boom? And the sizes adequate for wing spar reinforcement?
Ultimately, I'd like to get down to below the 250 gram limit so as to have at least one aircraft that I can legally fly without permission from the FAA (and will give me some nice soaring capabilities), but this is a serious challenge. I'm pretty sure a 2 meter wingspan is probably out of the question, so I'm aiming for a 60" wingspan. My current design is a combination of the Armin wing and FT techniques. It is tapered towards the ends, so provides some additional challenges with the main spar. My first prototype wing weighs in at just over 180 grams, so is already a substantial portion of the limit before even adding the fuselage, tail, and electronics.
To get that weight down, it looks like I'll have to remove paper from both sides of the foamboard before construction (which seems to be almost half of the weight of DTFB), then use packing tape for covering the outside. A carbon rod might be needed for reinforcing the spar, but I'll have to see how it does without, first.
I'll post pictures as it comes together....
Thanks!
Trying my hand at scratch building a plane of my own design of the sort seen here:
http://www.flitetest.com/articles/300-g-plane-design-80-mins-with-1600-mah-battery
Along with learning how to minimize weight by construction techniques, I need to learn to use new materials -- specifically the carbon fiber tubes and rods.
I'm trying to gauge what size tube would be needed for a ~30" tail boom for a 60" wingspan aircraft -- minimizing weight, while keeping it strong enough to survive flight (and not flex mid-flight). Looking at all the various sources on line, I can't get a good feel for what size and wall thickness will meet my needs.
Can anyone offer any suggestions or guidance on selecting the right size for a tail boom? And the sizes adequate for wing spar reinforcement?
Ultimately, I'd like to get down to below the 250 gram limit so as to have at least one aircraft that I can legally fly without permission from the FAA (and will give me some nice soaring capabilities), but this is a serious challenge. I'm pretty sure a 2 meter wingspan is probably out of the question, so I'm aiming for a 60" wingspan. My current design is a combination of the Armin wing and FT techniques. It is tapered towards the ends, so provides some additional challenges with the main spar. My first prototype wing weighs in at just over 180 grams, so is already a substantial portion of the limit before even adding the fuselage, tail, and electronics.
To get that weight down, it looks like I'll have to remove paper from both sides of the foamboard before construction (which seems to be almost half of the weight of DTFB), then use packing tape for covering the outside. A carbon rod might be needed for reinforcing the spar, but I'll have to see how it does without, first.
I'll post pictures as it comes together....
Thanks!