Originally posted by Elapid
how does it compare with pre-fab tubing from a cost per foot standpoint after all the supplies are purchased and construction time considered?
The cost is most likely similar, but may be higher or lower in some cases. Most commerical carbon tubing compaines are dealing with thousands of feet of tubing, and thus benefit from the mass market manufacturing techniques. However our product gives you a choice on how you to fullfill your tubing needs. If your concerned about the mass of the tube, or the strength of the tube you can ultizae different amounts of carbon and other materials to fit your needs exactly. I.e you can custom fit each tube/rocket airframe to your needs. Need to go mach 4 and 30,000 ft, Aerosleeve tubing can do that. Need to be comparable in weight to standard paper/LOC style tubing, but have much more stregnth (especially in the key direction, compression)
Originally posted by Elapid
how much will it cost me to make a 3' tube compared to the $53.00 (est) commercially available tube, and how will it compare structurally?
if it's a lot cheaper, or structurally superior, i'm on board!
It depends on how many layers of Aerosleeves you intend to use, what core material (if any) and if you plan to laminate or create full compoiste tubing.
1 yard of 2.5 " carbon (which will fit on 3" tubes with a 25% decrease in length) is $23.39.
1 yard of 3" fiberglass $12.99
You can figure out the price of the tube
you want to create.. Ad $1-2 per foot for epoxy.
I dislike recommending that you ever make a tube from one material. When you combine materials (and hence a composite within a composite) you will come out with a better result. Oblivosuly using a core material (honeycomb, Baltek/Coremat) or similar will result in the best end result, but this is difficult to do. You can intimate using a "true" core material with the use of fiberglass.. Fiberglass is alright as a tubing material by itself, but even better when pared with carbon. The carbon gives the laminate is stiffness and some strength, the fiberglass gives a lot more stregth and lets you ultize the carbon where it will be ultized the most, on the outside of the tube where the forces associated with loading are most pronounced. Think about why I -beams are better than straight beams..
Also, a inner layer of paper tubing is an excellent choice, especially for min diameter applications. The paper provides a lot of stiffness, plus a good amount of thermal insulation, important for long burning motors.
Also, don't ever confuse "stiffness" with strengh. Even because you maybe be able to "squeeze" the end of the tube, this does not mean the tube is "weak" and not strong. I've seen many rockets fly with tubes you can ovalize by squeezing fairly lightly. They've all held up during flight and even more impact prone landing. I'd rather have a tube that flexes some during loading, than one that will simply shatter when loaded in excess. (phenolic) Also, how many times do rockets ever enconter "squeezing forces" on the airframe ? Pretty much never. Its all compression and some torsion.
I've personally crashed a number of rockets that used composite airframes, some with aerosleeves. The amount of damage sustained by the airframe is almost always never. Likewise, how many phenolic/fillamentwound/paper just shatter on impact ? If you increase the time of impact, your overall loading force goes way down.. Cars are made with crumple zones and airbags for exactly that reason.. Rockets are starting to ultize the same ideas.
Nick Anderson
https://www.aerosleeves.com