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Space Grant Consortium - University of Wisconsin - Green Bay

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Background and Context:<br />

Student Rocket Design Competition<br />

“Rocky Mountain Miners”<br />

Brian Mortensen, Jon Neujahr, Ryan May<br />

Milwaukee School <strong>of</strong> Engineering<br />

Milwaukee, WI<br />

The rocket was designed for the 2009 <strong>Wisconsin</strong> <strong>Space</strong> Grand <strong>Consortium</strong> collegiate<br />

rocket competition. The objective <strong>of</strong> the competition is to construct a boosted dart rocket and<br />

attain the highest altitude. The boosted dart rocket consists <strong>of</strong> two parts. The first part is the<br />

booster, which is powered by an I-435 motor. Secondly, the dart is carried by the booster until<br />

the thrust from the motor ends. At this point, the dart flies as a projectile until apogee is<br />

achieved. There was no experience from any <strong>of</strong> the members <strong>of</strong> the team in rocketry.<br />

Procedure and Methods:<br />

The dart had three clipped delta<br />

fiberglass fins evenly spaced around the<br />

bottom <strong>of</strong> the dart’s airframe. The<br />

specific shape <strong>of</strong> the fins provide a<br />

reduction <strong>of</strong> any unnecessary drag on<br />

the dart while maintaining a stable flight<br />

with the CP lower than the CG.<br />

Recovery system <strong>of</strong> the dart<br />

A parachute with a diameter <strong>of</strong> 18 inches,<br />

0.5 inch wide climbing webbing, and a<br />

flame retardant cloth were used for the<br />

recovery <strong>of</strong> the dart. The flame retardant<br />

cloth served as a firewall. After apogee is<br />

achieved, the altimeter signals an explosive<br />

charge to separate the dart, and the<br />

parachute is deployed from the rocket.<br />

The dart is separated right above the<br />

electronics storage bay as shown in Figure<br />

2. One end <strong>of</strong> the webbing was attached to<br />

the top <strong>of</strong> the electronics bay; the other end<br />

was attached to the bottom <strong>of</strong> the nose<br />

cone.<br />

Figure 1: Dimensions <strong>of</strong> the Dart Fins<br />

Figure 2: Recovery for the Dart<br />

Funding for competition provided by: <strong>Wisconsin</strong> <strong>Space</strong> <strong>Grant</strong> <strong>Consortium</strong><br />

33<br />

Sweep = 3.5 in<br />

T.C = 2.5 in<br />

Span = 3.25 in

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