say i had some source of propulsion- whether it be compressed air, CO2, or a rocket engine, how can i calculate out how much weight it will be able to lift how high?
Thanks
calculating thrust/lift help please
- mark.f
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Well, in flight, you could calculate theoretical thrust (with the absence of an atmosphere) using inertia of the exhaust gases, which could again be guesstimated by stoichiometry and gas flow through a fixed orifice, but other than that basic attempt I'd say it's beyond both mine and your skill-level.
- homedepotpro
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well, you could measure how fast it accelerated an object with a known mass. then you know how much the force its created, you calculate its lift against the force of gravity which is 9.8 m/s^2. Have you taken and higher level science classes?

You can experimentally record it by putting it upside down on a scale.
@homedepotpro
Isn't he trying to figure out what its lift is? I like the scale idea. If you have seen mythbusters they use a light stand thing with an arm to hold the rocket out and some sort of force gauge underneath.
BTW how much does gravity change as you go up in altitude. If its anything significant that could really affect your answer.
Isn't he trying to figure out what its lift is? I like the scale idea. If you have seen mythbusters they use a light stand thing with an arm to hold the rocket out and some sort of force gauge underneath.
BTW how much does gravity change as you go up in altitude. If its anything significant that could really affect your answer.
mobile chernobyl wrote:I can shoot a Canuter Valve off my '82 Chevy Ram F150 AT LEAST 3/4 Mile with 'ma cannon made of soup cans duct taped together, then I just squirt some bacardi 151 in the chamber and hold up my cigarrete lighta and WHOOSH! That thing flies at least 3/4 mile
Yes, such a thing is possible, but it's really more a job for a computer simulation than some back of the envelope scratchings - although that could suffice.
I suggest getting on the line to D_Hall, as he's the aeronautical engineer.
I suggest getting on the line to D_Hall, as he's the aeronautical engineer.
Does that thing kinda look like a big cat to you?
- jimmy101
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If compresseed air or CO2 is your energy source then you should add water as the "ejected mass". A Google search should turn up thrust calculators for water rockets, for example;
http://www.et.byu.edu/~wheeler/benchtop/sim.php
http://physics.gallaudet.edu/tools/scwatroc.html
http://findarticles.com/p/articles/mi_q ... _n17172742
http://www.sciencebits.com/taxonomy/term/6 (scroll down a bit)
For Estes rocket engines a little physics is all you should need. The rockets are rated by the total impulse and pulse length. I'm sure a Google search will turn up a ballistics calculator for Estes engines.
If you are homebrewing your engines with a solid propellant you need to measure the impulse and burn time of the engine. Again, Google will, I'm sure, find everything you need to know.
http://www.et.byu.edu/~wheeler/benchtop/sim.php
http://physics.gallaudet.edu/tools/scwatroc.html
http://findarticles.com/p/articles/mi_q ... _n17172742
http://www.sciencebits.com/taxonomy/term/6 (scroll down a bit)
For Estes rocket engines a little physics is all you should need. The rockets are rated by the total impulse and pulse length. I'm sure a Google search will turn up a ballistics calculator for Estes engines.
If you are homebrewing your engines with a solid propellant you need to measure the impulse and burn time of the engine. Again, Google will, I'm sure, find everything you need to know.
