Respuesta :
1) Find the SI constant A.
Fx = A(t^2)
t = 1.25 s => Fx = A(1.25^2) => A = Fx / (1.25^2) = 781.25N / (1.25^2) s^2 = 500N/s^2
A = 500 N/s^2
2) What impulse does the engine exert on the rocket during the 1.50s interval starting 2.00s after the engine was fired?
I = Integral of Fx * dt from t = 2.0 s to t = 3.5 s
I = Integral of A(t^2)dt from t = 2.0s to t = 3.5s
I = 500(t^3) / 3 from t = 2.0 s to t = 3.5s
I = [500/3]* [(3.5s)^3 - (2.0s)^3 ] = 5812.5 N*s
3) By how much does the rocket's velocity change during this interval?
I = momentum change ; constant mass => m* velocity change =>
velocity change = I / m = 5812.5 N*s / 2250kg = 2.58 m/s
Fx = A(t^2)
t = 1.25 s => Fx = A(1.25^2) => A = Fx / (1.25^2) = 781.25N / (1.25^2) s^2 = 500N/s^2
A = 500 N/s^2
2) What impulse does the engine exert on the rocket during the 1.50s interval starting 2.00s after the engine was fired?
I = Integral of Fx * dt from t = 2.0 s to t = 3.5 s
I = Integral of A(t^2)dt from t = 2.0s to t = 3.5s
I = 500(t^3) / 3 from t = 2.0 s to t = 3.5s
I = [500/3]* [(3.5s)^3 - (2.0s)^3 ] = 5812.5 N*s
3) By how much does the rocket's velocity change during this interval?
I = momentum change ; constant mass => m* velocity change =>
velocity change = I / m = 5812.5 N*s / 2250kg = 2.58 m/s
1) The value of the constant [tex]A[/tex] in SI units is [tex]\boxed{500\,{{\text{N}} \mathord{\left/{\vphantom {{\text{N}} {{{\text{s}}^{\text{2}}}}}}\right.\kern-\nulldelimiterspace} {{{\text{s}}^{\text{2}}}}}}[/tex].
2) The impulse imparted by engine on the rocket during [tex]2.00\,{\text{s}}[/tex] to [tex]3.50\,{\text{s}}[/tex] is [tex]\boxed{5812.5\,{\text{N}} \cdot {\text{s}}}[/tex].
3) The change in velocity of the rocket during the interval [tex]2.00\,{\text{s}}[/tex] to [tex]3.50\,{\text{s}}[/tex] is [tex]\boxed{2.58\,{{\text{m}} \mathord{\left/{\vphantom{{\text{m}} {\text{s}}}} \right.\kern-\nulldelimiterspace} {\text{s}}}}[/tex].
Explanation:
Part (1):
The force acting on the rocket is given as:
[tex]{F_x} = A{t^2}[/tex]
Since the magnitude of force experienced by the rocket is [tex]781.25\,{\text{N}}[/tex] at the instant [tex]t = 1.25\,{\text{s}}[/tex], the value of constant [tex]A[/tex] is calculated as:
[tex]\begin{aligned}781.25&= A{\left( {1.25} \right)^2}\\ A&= \frac{{781.25}}{{1.5625}}\\&= 500\,{{\text{N}} \mathord{\left/ {\vphantom {{\text{N}} {{{\text{s}}^{\text{2}}}}}} \right.\kern-\nulldelimiterspace} {{{\text{s}}^{\text{2}}}}}\\\end{aligned}[/tex]
Thus, the value of the constant in SI units is [tex]\boxed{500\,{{\text{N}} \mathord{\left/{\vphantom {{\text{N}}{{{\text{s}}^{\text{2}}}}}}\right.\kern-\nulldelimiterspace} {{{\text{s}}^{\text{2}}}}}}[/tex].
Part (2):
The impulse imparted by the engine is the amount of force exerted in the small interval of time. The impulse imparted by the engine on the rocket during [tex]2.00\,{\text{s}}[/tex] to [tex]3.50\,{\text{s}}[/tex] is given by:
[tex]I=\int\limits_{t = 2.0}^{3.5}{F \cdot dt}[/tex]
Substitute the expression of the force in the above expression of impulse.
[tex]\begin{aligned}I&= \int\limits_{t = 2.0}^{3.5} {A{t^2}dt}\\&= A\left[ {\frac{{{t^3}}}{3}} \right]_{2.0}^{3.5}\\&= \frac{{500}}{3}\left[ {{{\left( {3.5}\right)}^3} - {{\left( {2.0} \right)}^3}} \right]\\&= 5812.5\,{\text{N}}\cdot {\text{s}}\\\end{aligned}[/tex]
Thus, the imparted by engine on the rocket during [tex]2.00\,{\text{s}}[/tex] to [tex]3.50\,{\text{s}}[/tex] is [tex]\boxed{5812.5\,{\text{N}} \cdot {\text{s}}}[/tex].
Part (3):
According to the impulse-momentum theorem, the impulse imparted by the engine is equal to the change in momentum of the rocket. It is expressed as:
[tex]\begin{aligned}I&=\Deltap\hfill\\I&=m\times\Deltav \hfill\\\end{aligned}[/tex]
The mass of rocket is [tex]2250\,{\text{kg}}[/tex] and the impulse imparted by the engine is [tex]5812.5\,{\text{N}} \cdot {\text{s}}[/tex].
Substitute the values in the above expression.
[tex]\begin{aligned} 5812.5 &= 2250\times\Delta v\\\Delta v&= \frac{{5812.5}}{{2250}}\,{{\text{m}}\mathord{\left/{\vphantom {{\text{m}} {\text{s}}}} \right.\kern-\nulldelimiterspace} {\text{s}}}\\&= 2.58\,{{\text{m}}\mathord{\left/{\vphantom{{\text{m}} {\text{s}}}} \right.\kern-\nulldelimiterspace} {\text{s}}}\\\end{aligned}[/tex]
Thus, the change in velocity of the rocket due to the impulse imparted by the engine is
[tex]\boxed{2.58\,{{\text{m}} \mathord{\left/{\vphantom {{\text{m}} {\text{s}}}}\right.\kern-\nulldelimiterspace} {\text{s}}}}[/tex]
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Answer Details:
Grade: High School
Subject: Physics
Chapter: Impulse-momentum theorem
Keywords: Impulse imparted, the engine exerts, 1.50s interval, starting at 2.00s, rocket’s velocity change, magnitude of force, 2250 kg, in outer space fires an engine, impulse-momentum theorem.