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Given a long, thin rod of uniform density, in space, at rest relative to our reference frame. Length ''L'', mass ''M''. A very small, light rocket can be attached to the rod at anywhere along its length, providing a constant force ''F''. ''F<sub>0</sub>'' is applied at the center (''x''=0); ''F<sub>1</sub>'' is along the end (''x''=''L''/2). ''K'' is the kinetic energy; ''K<sub>t</sub>'' is the translational kinetic energy, and ''K<sub>r</sub>'' is the rotational kinetic energy.

==F<sub>0</sub>: x = 0==
There will be no rotation.

<math>F = ma</math>

<math>F_0 = Ma</math>

<math>a = \frac{F_0}{M}</math>

<math>v(t) = at</math>

<math>K_t(t) = {1 \over 2}m^2</math>

<math>
K_t(t) = {1 \over 2}M(at)^2
= {1 \over 2}M{\left( \frac{F_0 t}{M} \right)}^2
= \frac{F_0^2 Mt^2}{2M^2}
= \frac{F_0^2 t^2}{2M}
</math>

Test:
<math>
\frac{F_0^2 t^2}{2M} \rightarrow \frac{\left( \frac{kg \cdot m}{s^2} \right)^2 s^2}{kg}
= \frac{kg^2 \cdot m^2 \cdot s^2}{s^4 \cdot kg}
= \frac{kg \cdot m^2}{s^2}
</math>

<math>K_t(t) = \frac{F_0^2 t^2}{2M}</math>

==F<sub>1</sub>: x = L / 2==
There will be some rotation.

<math>\tau_i
= F_i l
= F_1 \frac{L}{2}
</math>

<math> \tau = I \alpha</math>

<math>F_1 \frac{L}{2} = \left( \frac{1}{12} ML^2 \right) \alpha
</math>

<math>
\alpha = \frac{F_1 \frac{L}{2}}{\frac{1}{12} ML^2}
= \frac{12F_1 L}{2ML^2}
= \frac{6F_1}{ML}
</math>

<math>\omega (t) = \alpha t</math>

<math>
K_r(t) = \frac{1}{2}I^2
=\frac{1}{2} \left( \frac{1}{12} ML^2 \right) \left( \alpha t \right)^2
=\frac{1}{2} \left( \frac{1}{12} ML^2 \right) \left^2
=\frac{36ML^2 F_1^2 t^2}{24M^2 L^2}
=\frac{3F_1^2 t^2}{2M}
</math>

Latest revision as of 03:04, 1 May 2013