pkh
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- Joined
- Oct 21, 2005
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Hi guys... I'm new to this forum, and model rocketry, and I wanted to run my latest "experimental" project by you to get comments/suggestions...
I'm planning to build a rocket with moveable control surfaces on the fins, so that the rocket can be guided back to the launch area while it descends. It won't be a rocket boosted glider, really, since there will be no wing, just moveable fins. The idea is to come in with a relatively fast, steep descent and try to flare up to a horizontal position for a belly landing.
I plan to use a Hitec Feather micro receiver, two HS-55 micro servos, and a small 4 cell 2/3AAA batt pack. I'm going to start with an Estes Patriot kit (BT-60 body tubes) and modify it. I'll custom make 3 large balsa fins, two of which will have hinged control surfaces on them (these will act as "elevons" during descent). I also plan to install a "firewall" and make a vented section in the body tube to vent the heat and gases from the "burn through" on unplugged engines. I'll build the Patriot with a D sized engine mount, since this rocket will weigh close to 8oz. I plan to fly D11-Ps in it, which should get me up to about 600ft, but for the first flight I'm planning on a C11-0, which should only take it up to about 300ft.
My primary concerns so far are:
1) Will the hinged control surfaces hold up to the 90-140mph top speeds? CA hinges and hinge tape are the common methods of hinging very lightweight aircraft control surfaces, but those aircraft typicall don't reach these high speeds!
2) How will the stability be affected by only having fins at 0, 90, & 270 degrees around the body tube (see attached diagram... no fin at 180 degrees so I can belly land it). I'm guessing that the drag caused by the 0 degree fin will cause the rocket to arc slightly in that direction, since there is no fin at 180 degrees to offset the drag.
3) How to calculate the CP when the projected area with the 90 & 270 degree fins will give a CP further back than the projected area with just the 0 degree fin. Right now, I figure I'll just calculated the CP with just the 0 degree fin in the projected area to get the worst case stability factor.
Thanks for reading all of this... if you made it this far! Any comments and suggestions are welcome!
I'm planning to build a rocket with moveable control surfaces on the fins, so that the rocket can be guided back to the launch area while it descends. It won't be a rocket boosted glider, really, since there will be no wing, just moveable fins. The idea is to come in with a relatively fast, steep descent and try to flare up to a horizontal position for a belly landing.
I plan to use a Hitec Feather micro receiver, two HS-55 micro servos, and a small 4 cell 2/3AAA batt pack. I'm going to start with an Estes Patriot kit (BT-60 body tubes) and modify it. I'll custom make 3 large balsa fins, two of which will have hinged control surfaces on them (these will act as "elevons" during descent). I also plan to install a "firewall" and make a vented section in the body tube to vent the heat and gases from the "burn through" on unplugged engines. I'll build the Patriot with a D sized engine mount, since this rocket will weigh close to 8oz. I plan to fly D11-Ps in it, which should get me up to about 600ft, but for the first flight I'm planning on a C11-0, which should only take it up to about 300ft.
My primary concerns so far are:
1) Will the hinged control surfaces hold up to the 90-140mph top speeds? CA hinges and hinge tape are the common methods of hinging very lightweight aircraft control surfaces, but those aircraft typicall don't reach these high speeds!
2) How will the stability be affected by only having fins at 0, 90, & 270 degrees around the body tube (see attached diagram... no fin at 180 degrees so I can belly land it). I'm guessing that the drag caused by the 0 degree fin will cause the rocket to arc slightly in that direction, since there is no fin at 180 degrees to offset the drag.
3) How to calculate the CP when the projected area with the 90 & 270 degree fins will give a CP further back than the projected area with just the 0 degree fin. Right now, I figure I'll just calculated the CP with just the 0 degree fin in the projected area to get the worst case stability factor.
Thanks for reading all of this... if you made it this far! Any comments and suggestions are welcome!