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Space Grant Consortium - University of Wisconsin - Green Bay

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successfully fit the necessary components inside this size dart, but concluded the further<br />

reductions in size were not practical.<br />

The second major design objective for the dart was to ensure stability. Stability is <strong>of</strong> major<br />

importance in rocketry. As a rocket flies, all the drag forces and wind forces effectively act as<br />

though a single force is applied at one location—the center <strong>of</strong> pressure (CP). If the CP does not<br />

exactly coincide with the center <strong>of</strong> gravity (CG), then the resultant force causes rotation <strong>of</strong> the<br />

rocket about the CG. Three classes <strong>of</strong> flight stability depend on the relative positions <strong>of</strong> the CG<br />

and CP:<br />

1) CP is in front <strong>of</strong> CG: Rocket is unstable.<br />

2) CP is just behind the CG: Rocket is stable.<br />

3) CP is far behind CG: Rocket is over-stable.<br />

It is clear that case 2 is the most desirable. As a rule <strong>of</strong> thumb, a rocket with a CP that is located<br />

between 1 and 2 rocket diameters behind the CG falls into this category. Barrowman’s theory<br />

was used to approximate the CP <strong>of</strong> the rocket. This theory was submitted by James Barrowman<br />

as a practical means to compute a slender rocket’s center <strong>of</strong> pressure under general<br />

considerations (most prior theories involved detailed assumptions that made them invalid for the<br />

majority <strong>of</strong> applications). Avoiding such limiting assumptions, Barrowman’s theory applies to<br />

most slender rockets flying at subsonic speeds and low angles <strong>of</strong> attack. Barrowman found his<br />

theory’s predictions to be within 10% agreement <strong>of</strong> wind tunnel testing in most cases.<br />

The following scale drawings show the CPs and CGs <strong>of</strong> the dart. Note that the rocket falls in the<br />

stable range, where the CP is 1-2 calibers behind the CG.<br />

CG CP<br />

Figure 2: Scale drawing <strong>of</strong> 1.5 inch diameter dart showing CP and CG<br />

Entire Assembly The booster and dart cannot be designed individually; rather, they must<br />

operate in tandem and be designed with compatibility in mind. For the interface between the dart<br />

and booster, two design features are <strong>of</strong> great importance: the method <strong>of</strong> joining/separating, and<br />

the stability <strong>of</strong> the assembly.<br />

17

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