- #1
Adoniram
- 94
- 6
Hello All, a few friends of mine and I have devised the ridiculous idea that it would be fun to build a rocket that could do something like the popular weather balloon projects which achieve high altitude for cool visuals (via GoPro or similar). But we want to make it better/faster/cooler. The objectives are:
Some strategic goals are:
I think 2 and 3 will be a fun engineering project, and 4 will be somewhat costly and monumental, but my job is to focus primarily on # 1 for now. It has been a long time since I took CM, so I could use some help... This is what I need to account for (some things are redundant):
I've seen somewhat decently developed EOM for a or c, but never together. Incorporating b should really be something included with c.
If you know of any really well developed models for this, that include all 3, I would really appreciate it! The best I've seen so far, which only has one of those requirements, are here:
http://www.rocketmime.com/rockets/rckt_eqn.html#Method
and here:
http://web.mit.edu/16.unified/www/FALL/thermodynamics/notes/node103.html
Thanks!
ps: yes I know this will require legal hurdles as well, FAA rules, ITAR, etc...
- Rocket is actually swept-wing jet body with retractable wings (in for launch, out for return)
- Rocket achieves high altitude (>50,000 ft is the real goal)
- Uses arduino or similar to maintain both launch and return trajectory
- Flies to specified way points on return
- Takes super cool video
Some strategic goals are:
- Develop actual mathematical model to explore parameter space of weight and fuel vs max altitude
- Make simple robotic rocket (plain vanilla Estes with D or E engines) to test and program robotics for upward flight control (point straight up, don't roll, etc)
- Make simple robotic rocket with retractable wings to test return control
- Scale up to higher altitudes, eventually use more exotic fuels, etc
I think 2 and 3 will be a fun engineering project, and 4 will be somewhat costly and monumental, but my job is to focus primarily on # 1 for now. It has been a long time since I took CM, so I could use some help... This is what I need to account for (some things are redundant):
- a. Non-constant mass (obviously)
- b. Non-constant air pressure/density/temperature
- c. Drag
I've seen somewhat decently developed EOM for a or c, but never together. Incorporating b should really be something included with c.
If you know of any really well developed models for this, that include all 3, I would really appreciate it! The best I've seen so far, which only has one of those requirements, are here:
http://www.rocketmime.com/rockets/rckt_eqn.html#Method
and here:
http://web.mit.edu/16.unified/www/FALL/thermodynamics/notes/node103.html
Thanks!
ps: yes I know this will require legal hurdles as well, FAA rules, ITAR, etc...