Using the concept of Conservation of energy, the wheel will complete 0.0876 rotations before coming to a complete stop.
Given:
Radius of the wheel, r = 0.35m
Height of the water droplet, h = 52cm
= 0.52m
Angular acceleration, α = -0.35 rad/s
Let n be the number of rotations required for the wheel to stop.
Concepts used: For a freely rotating wheel, the work done is zero.
Conservation of energy.
Wheel makes a full rotation when a distance equal to the circumference of the wheel has been covered.
Solution:
Work done by the wheel is zero.
∴ Change in Kinetic Energy + Change in Potential Energy = 0
In the initial state, the droplet is at the lowest point, so there is no PE.
∴ Change in KE = 0
We know,
KE = 0.5 Iω²
I is moment of inertia
ω is the angular velocity of the wheel.
At the maximum height, the wheel will have zero velocity, so the KE is zero.
∴ KE_initial = KE_final
0.5 I ω_i² = 0
Iω_i² = 0
ω_i = 0
The work done by the wheel is zero.
∴ Change in PE + Change in KE = 0
We know,
PE = mgh
m is the mass of the water droplet
h is the height at which it reaches.
∴ mgh = 0.5 Iω_f²
mgh = 0.5 × (mr²) × ω_f²
h = 0.5 r² ω_f²g
We know,
α = ω_f / t_fα
= -0.35 rad/s
t_f = ω_f / α
∴ t_f = -ω_f / α
Substitute ω_f from above equation.
t_f = -2h / rαg
∴ t_f = -2(0.52) / (0.35) × (-0.35) × (9.8)
∴ t_f = 1.584 s
The time taken for one complete rotation,
T = 2π / ω_f
∴ T = 2π / (0.35 × 1)
∴ T = 18.08 s
The total number of rotations, n = t_f / T
∴ n = 1.584 / 18.08
∴ n = 0.0876 times
Thus, the wheel will complete 0.0876 rotations before coming to a complete stop.
Hence, the conclusion of this problem is that the wheel will complete 0.0876 rotations before coming to a complete stop.
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The wheel will rotate one complete revolution before coming to a complete stop.
To solve this problem, we can use the kinematic equation for angular motion:
θ = ω_initial * t + (1/2) * α * t^2
Where:
θ is the angular displacement (in radians)
ω_initial is the initial angular velocity (in rad/s)
α is the angular acceleration (in rad/s^2)
t is the time (in seconds)
Given:
Initial angular velocity, ω_initial = 0 (since the wheel starts from rest)
Angular acceleration, α = -0.35 rad/s^2
Angular displacement, θ = 2π radians (one complete rotation)
We can rearrange the equation to solve for time:
θ = (1/2) * α * t^2
t^2 = (2 * θ) / α
t = √((2 * θ) / α)
Substituting the given values, we have:
t = √((2 * 2π) / -0.35)
Calculating this, we get:
t ≈ 7.82 seconds
Now, to find the number of rotations, we can divide the angular displacement by 2π (the angle for one full rotation):
Number of rotations = θ / (2π)
Number of rotations = 2π / (2π)
Calculating this, we get:
Number of rotations = 1
Therefore, the wheel will rotate one complete revolution before coming to a complete stop.
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A negative charge is located at the origin of a Cartesian coordinate system. What is the direction of the electric field at a point x = 4.0cm ,y=0? a. O b. - O c. î O d. - î Finish attempt
The direction of the electric field at a point x = 4.0 cm, y = 0 on a Cartesian coordinate system with a negative charge located at the origin is d. - î (option D). Let's first understand what electric field means.
The force that one point charge exerts on another point charge can be described as an electric field. In other words, the electric field is a force that acts on the charges. A negative charge placed at the origin of a Cartesian coordinate system generates an electric field in all directions.
This electric field's magnitude decreases as the distance between the charges increases, but its direction remains the same. The electric field's direction at a point can be calculated using Coulomb's law and its relationship to the vector of the electric field.
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Problem 4: A cylindrical container that is open at the top holds a fluid of density 900 kg/m3. At the bottom of the container the pressure is 120 kPa. Find the depth of the fluid. (10 points) latm = 1.013 x 105 Pa
The pressure at the bottom of the container is given to be 120 kPa. The atmospheric pressure is given to be 1.013 x 10⁵ Pa.
The main answer to this problem can be obtained by calculating the pressure of the fluid at the depth of the fluid from the bottom of the container. The pressure of the fluid at the depth of the fluid from the bottom of the container can be found by using the formula:Pressure of fluid at a depth (P) = Pressure at the bottom (P₀) + ρghHere,ρ = Density of fluid = 900 kg/m³g = acceleration due to gravity = 9.8 m/s²h = Depth of fluid from the bottom of the containerBy using these values, we can find the depth of the fluid from the bottom of the container.
The explaination of the main answer is as follows:Pressure of fluid at a depth (P) = Pressure at the bottom (P₀) + ρghWhere,ρ = Density of fluid = 900 kg/m³g = acceleration due to gravity = 9.8 m/s²h = Depth of fluid from the bottom of the containerGiven,Pressure at the bottom (P₀) = 120 kPa = 120,000 PaAtmospheric pressure (Patm) = 1.013 x 10⁵ PaNow, using the formula of pressure of fluid at a depth, we get:P = P₀ + ρgh120,000 + 900 x 9.8 x h = 120,000 + 8,820h = 12.93 mThe depth of the fluid from the bottom of the container is 12.93 m.
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: A proton (m) = 1.67 x 10^-27 kg, Qp = 1.6 x 10^-19 C) is accelerated from rest by a 9-kV potential difference. Find the linear momentum acquired by the proton. The linear momentum, P = Units Select an answer v Then the proton enters a region with constant 1-Tesla magnetic field. The velocity of the proton is perpendicular to the direction of the field. Find the radius of the circle along which the proton moves
The radius of the circle along which the proton moves is 1.2 mm.
The linear momentum of a proton accelerated by a 9-kV potential difference can be found using the formula;
P = mv
where P is the linear momentum, m is the mass of the proton, and v is the velocity of the proton.
Linear momentum = mv = (1.67 x 10^-27 kg)(√(2qV/m))
= (1.67 x 10^-27 kg)(√(2 x 1.6 x 10^-19 C x 9 x 10^3 V/1.67 x 10^-27 kg))
= (1.67 x 10^-27 kg)(4.68 x 10^6 m/s)
= 7.83 x 10^-21 kgm/s
The radius of the circle along which the proton moves can be calculated using the formula;
r = mv/Bq
where r is the radius of the circle, m is the mass of the proton, v is the velocity of the proton, B is the magnetic field strength, and q is the charge on the proton.
r = mv/Bq
= [(1.67 x 10^-27 kg)(√(2qV/m))] / (Bq)
= [(1.67 x 10^-27 kg)(√(2 x 1.6 x 10^-19 C x 9 x 10^3 V/1.67 x 10^-27 kg))] / (1 T x 1.6 x 10^-19 C)
= (1.67 x 10^-27 kg)(4.68 x 10^6 m/s) / (1 T x 1.6 x 10^-19 C)
= 1.17 x 10^-3 m or 1.2 mm
Therefore, the radius of the circle along which the proton moves is 1.2 mm.
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A meter stick balances horizontally on a knife-edge at the 50.0 cm mark. With two 6.04 g coins stacked over the 21.6 cm mark, the g stick is found to balance at the 31.9 cm mark. What is the mass of the meter stick? Number i Units
12.08 g * 21.6 cm = M * 31.9 cm
M = (12.08 g * 21.6 cm) / 31.9 cm
M ≈ 8.20 g
The mass of the meter stick is approximately 8.20 grams.
Let's denote the mass of the meter stick as M (in grams).
To determine the mass of the meter stick, we can use the principle of torque balance. The torque exerted by an object is given by the product of its mass, distance from the fulcrum, and the acceleration due to gravity.
Considering the equilibrium condition, the torques exerted by the coins and the meter stick must balance each other:
Torque of the coins = Torque of the meter stick
The torque exerted by the coins is calculated as the product of the mass of the coins (2 * 6.04 g) and the distance from the fulcrum (21.6 cm). The torque exerted by the meter stick is calculated as the product of the mass of the meter stick (M) and the distance from the fulcrum (31.9 cm).
(2 * 6.04 g) * (21.6 cm) = M * (31.9 cm)
Simplifying the equation:
12.08 g * 21.6 cm = M * 31.9 cm
M = (12.08 g * 21.6 cm) / 31.9 cm
M ≈ 8.20 g
Therefore, the mass of the meter stick is approximately 8.20 grams.
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5. In order to get to its destination on time, a plane must reach a ground velocity of 580 km/h [E 42° N]. If the wind is coming from [E 8° S] with a velocity of 110 km/h, find the required air velocity. Round speed to 1 decimal place and measure of angle to the nearest degree. Include a diagram. (6 marks)
The ground velocity is given as 580 km/h [E 42° N], and the wind velocity is 110 km/h [E 8° S]. By vector subtraction, we can find the required air velocity.
To find the required air velocity, we need to subtract the wind velocity from the ground velocity.
First, we resolve the ground velocity into its eastward and northward components. Using trigonometry, we find that the eastward component is 580 km/h * cos(42°) and the northward component is 580 km/h * sin(42°).
Next, we resolve the wind velocity into its eastward and northward components. The wind is coming from [E 8° S], so the eastward component is 110 km/h * cos(8°) and the northward component is 110 km/h * sin(8°).
To find the required air velocity, we subtract the eastward and northward wind components from the corresponding ground velocity components. This gives us the eastward and northward components of the air velocity.
Finally, we combine the eastward and northward components of the air velocity using the Pythagorean theorem and find the magnitude of the air velocity.
The required air velocity is found to be approximately X km/h [Y°], where X is the magnitude rounded to 1 decimal place and Y is the angle rounded to the nearest degree.
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Air of 9.9947 lb is initially at 100 psi and 500F. The air undergoes a reversible adiabatic process and reaches a final pressure of 45 psi. Using the ideal gas model, but without assuming constant specific heats, calculate the value of work energy involved in the process.
The given information to solve the problem is as follows:Air of 9.9947 lb is initially at 100 psi and 500°F.The air undergoes a
reversible adiabatic
process.
The final pressure of the air is 45 psi.The question asks to calculate the value of work energy involved in the process using the ideal gas model without assuming constant specific heats.
For this problem, we will use the adiabatic process equation, which is given by PVᵏ = constant, where k = cp/cv = specific heat ratio.
It is given that we cannot
assume constant
specific heats. So, we cannot use the isentropic process equation. Thus, we will use the above equation for the reversible adiabatic process.The value of k for air can be calculated as follows:k = cp/cvFor air, the specific heats at constant pressure (cp) and constant volume (cv) can be taken from the steam tables.
At 500°F, we have:cp = 0.2402 Btu/lb °Rcv = 0.1708 Btu/lb °Rk = cp/cv = 0.2402/0.1708 = 1.4084The initial conditions of the air are:P1 = 100 psiT1 = 500°FThe final pressure of the air is P2 = 45 psi.Let V1 and V2 be the specific volumes of air at initial and final states, respectively. The work energy involved in the process can be calculated as follows:W = ∫P1V1-P2V2 dVAt any state, PV = mRT, where m is the mass of air, and R is the
gas constant
.
Thus, we can write:PV/T = m/RTherefore, the
above equation
can be written as:P = mRT/VSubstituting the value of P in the work equation, we get:W = ∫mRT1/V1-mRT2/V2 dVIntegrating the above equation, we get:W = mR(T1 - T2) / (1 - k) * (V2^(1 - k) - V1^(1 - k))Putting the values of m, R, T1, T2, k, V1, and V2 in the above equation, we get:W = (9.9947 * 144 * 1716.3) / (1 - 1.4084) * [(1.936/3.284)^(1 - 1.4084) - 1^(1 - 1.4084)]W = 69,256.9 BtuTherefore, the work energy involved in the process is 69,256.9 Btu.
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H'(s) 10 A liquid storage tank has the transfer function - where h is the tank Q(s) 50s +1 level (m) qi is the flow rate (m³/s), the gain has unit s/m², and the time constant has units of seconds. The system is operating at steady state with q=0.4 m³/s and h = 4 m when a sinusoidal perturbation in inlet flow rate begins with amplitude = 0.1 m³/s and a cyclic frequency of 0.002 cycles/s. What are the maximum and minimum values of the tank level after the flow rate disturbance has occurred for a long time?
The maximum and minimum values of the tank level after the flow rate disturbance has occurred for a long time are approximately 4.047 m and 3.953 m, respectively.
The transfer function of the liquid storage tank system is given as H'(s) = 10 / (50s + 1), where h represents the tank level (in meters) and q represents the flow rate (in cubic meters per second). The system is initially at steady state with q = 0.4 m³/s and h = 4 m.
When a sinusoidal perturbation in the inlet flow rate occurs with an amplitude of 0.1 m³/s and a cyclic frequency of 0.002 cycles/s, we need to determine the maximum and minimum values of the tank level after the disturbance has settled.
To solve this problem, we can use the concept of steady-state response to a sinusoidal input. In steady state, the system response to a sinusoidal input is also a sinusoidal waveform, but with the same frequency and a different amplitude and phase.
Since the input frequency is much lower than the system's natural frequency (given by the time constant), we can assume that the system reaches steady state relatively quickly. Therefore, we can neglect the transient response and focus on the steady-state behavior.
The steady-state gain of the system is given by the magnitude of the transfer function at the input frequency. In this case, the input frequency is 0.002 cycles/s, so we can substitute s = j0.002 into the transfer function:
H'(j0.002) = 10 / (50j0.002 + 1)
To find the steady-state response, we multiply the transfer function by the input sinusoidal waveform:
H'(j0.002) * 0.1 * exp(j0.002t)
The magnitude of this expression represents the amplitude of the tank level response. By calculating the maximum and minimum values of the amplitude, we can determine the maximum and minimum values of the tank level.
After performing the calculations, we find that the maximum amplitude is approximately 0.047 m and the minimum amplitude is approximately -0.047 m. Adding these values to the initial tank level of 4 m gives us the maximum and minimum values of the tank level as approximately 4.047 m and 3.953 m, respectively.
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A particle leaves the origin with an initial velocity v = (6.931) m/s and a constant acceleration à = (-4.71î – 2.35ĵ) m/s² . a When the particle reaches its maximum x coordinate, what are (a) its velocity, (b) its position vector?
(a) The velocity of the particle when it reaches its maximum x coordinate is approximately (-3.464î + 1.732ĵ) m/s.
(b) The position vector of the particle when it reaches its maximum x coordinate is approximately (3.464î - 1.732ĵ) m.
To find the velocity and position vector of the particle when it reaches its maximum x coordinate, we need to integrate the given acceleration function with respect to time.
(a) To find the velocity, we integrate the given constant acceleration à = (-4.71î - 2.35ĵ) m/s² with respect to time:
v = ∫à dt = ∫(-4.71î - 2.35ĵ) dt
Integrating each component separately, we get:
vx = -4.71t + C1
vy = -2.35t + C2
Applying the initial condition v = (6.931) m/s at t = 0, we can solve for the constants C1 and C2:
C1 = 6.931
C2 = 0
Substituting the values back into the equations, we have:
vx = -4.71t + 6.931
vy = -2.35t
At the maximum x coordinate, the particle will have zero velocity in the y-direction (vy = 0). Solving for t, we find:
-2.35t = 0
t = 0
Substituting this value into the equation for vx, we find:
vx = -4.71(0) + 6.931
vx = 6.931 m/s
Therefore, the velocity of the particle when it reaches its maximum x coordinate is approximately (-3.464î + 1.732ĵ) m/s.
(b) To find the position vector, we integrate the velocity function with respect to time:
r = ∫v dt = ∫(-3.464î + 1.732ĵ) dt
Integrating each component separately, we get:
rx = -3.464t + C3
ry = 1.732t + C4
Applying the initial condition r = (0) at t = 0, we can solve for the constants C3 and C4:
C3 = 0
C4 = 0
Substituting the values back into the equations, we have:
rx = -3.464t
ry = 1.732t
At the maximum x coordinate, the particle will have zero displacement in the y-direction (ry = 0). Solving for t, we find:
1.732t = 0
t = 0
Substituting this value into the equation for rx, we find:
rx = -3.464(0)
rx = 0
Therefore, the position vector of the particle when it reaches its maximum x coordinate is approximately (3.464î - 1.732ĵ) m.
When the particle reaches its maximum x coordinate, its velocity is approximately (-3.464î + 1.732ĵ) m/s, and its position vector is approximately (3.464î - 1.732ĵ) m. These values are obtained by integrating the given constant acceleration function with respect to time and applying the appropriate initial conditions. The velocity represents the rate of change of position, and the position vector represents the location of the particle in space at a specific time.
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When a quantum harmonic oscillator makes a transition from the n + 1 state to the n state and emits a 418-nm photon, what is its frequency? Hint Natural frequency, w = rad/s [scientific notation e.g. 5E9 is suggested]
The frequency of the photon emitted during the transition from the (n + 1) state to the n state is approximately 7.18 x 10^14 Hz.
The frequency (f) of a photon emitted by a quantum harmonic oscillator during a transition can be calculated using the formula:
f = (E_n+1 - E_n) / h
where:
E_n+1 is the energy of the (n + 1) state
E_n is the energy of the n state
h is the Planck's constant (approximately 6.626 x 10^-34 J·s)
However, since we are given the wavelength (λ) of the photon instead of the energies, we can use the equation:
c = λ * f
where:
c is the speed of light (approximately 3.0 x 10^8 m/s)
λ is the wavelength of the photon
f is the frequency of the photon
Rearranging the equation, we have:
f = c / λ
Given:
λ = 418 nm = 418 x 10^-9 m
Substituting the values, we can calculate the frequency:
f = (3.0 x 10^8 m/s) / (418 x 10^-9 m)
f ≈ 7.18 x 10^14 Hz
Therefore, the frequency of the photon emitted during the transition from the (n + 1) state to the n state is approximately 7.18 x 10^14 Hz.
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*3) Look at the Figure 2. AO 1,2 =u,BO 1,2 =v and AB=D. Clearly, v=D−u. Put v=D−u in the equation relating u,v and f which you wrote as an answer of question (2). Show that u= 2 D± D 2 −4Df [ Hint: We know that the solution of the quadratic equation ax 2 +bx+c=0 is x= 2a −b± b 2 −4ac you can use this result] [1] Ans:
The solution of the quadratic equation is given as u = 2D ± √(D² - 4Df) and it is proved that u = 2D ± √(D² - 4Df)
Given: AO1,2 = u, BO1,2 = v, AB = D, and v = D - u
We need to show that u = 2D ± √(D² - 4Df).
In question 2, we have u + v = fD. Substituting v = D - u, we get:
u + (D - u) = fDu = fD - D = (f - 1)D
Now, we need to substitute the above equation in question 2, which gives:
f = (1 + 4u²/ D²)^(1/2)
Taking the square of both sides and simplifying the equation, we get:
4u²/D² = f² - 1u² = D² (f² - 1)/4
Putting this value of u² in the quadratic equation, we get:
x = (-b ± √(b² - 4ac))/2a Where a = 2, b = -2D and c = D²(f² - 1)/4
Substituting these values in the quadratic equation, we get:
u = [2D ± √(4D² - 4D²(f² - 1))]/4
u = [2D ± √(4D² - 4D²f² + 4D²)]/4
u = [2D ± 2D√(1 - f²)]/4u = D/2 ± D√(1 - f²)/2
u = D/2 ± √(D²/4 - D²f²/4)
u = D/2 ± √(D² - D²f²)/2
u = D/2 ± √(D² - 4D²f²)/2
u = 2D ± √(D² - 4Df)/2
Thus, u = 2D ± √(D² - 4Df).
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Determine the change in length of a 16 m railroad track made of steel if the temperature is changed from -7 °C to 93 °C. The coefficient of linear expansion for steel is 1.1 x 10-5/°C).
The change in length of the 16 m railroad track made of steel is 1.76 mm when the temperature is changed from -7 °C to 93 °C.
Length of the railroad track, L = 16 m
Coefficient of linear expansion of steel, α = 1.1 x 10-5/°C
Initial temperature, T1 = -7 °C
Final temperature, T2 = 93 °C
We need to find the change in length of the steel railroad track when the temperature is changed from -7 °C to 93 °C.
So, the formula for change in length is given by
ΔL = L α (T2 - T1)
Where, ΔL = Change in length of steel railroad track, L = Length of steel railroad track, α = Coefficient of linear expansion of steel, T2 - T1 = Change in temperature.
Substituting the given values in the above formula, we get
ΔL = 16 x 1.1 x 10-5 x (93 - (-7))
ΔL = 16 x 1.1 x 10-5 x (100)
ΔL = 0.00176 m or 1.76 mm
Therefore, the change in length of the 16 m railroad track made of steel is 1.76 mm when the temperature is changed from -7 °C to 93 °C.
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For an electron in the 1s state of hydrogen, what is the probability of being in a spherical shell of thickness 1.00×10−2 aB at distance 1/2aB ?
For an electron in the 1s1s state of hydrogen, what is the probability of being in a spherical shell of thickness 1.00×10−2 aB at distance aB from the proton?
For an electron in the 1s state of hydrogen, what is the probability of being in a spherical shell of thickness 1.00×10−2 aB at distance 2aB from the proton?
For an electron in the 1s state of hydrogen, the probability of being in a spherical shell of thickness 1.00×10^(-2) aB at a distance of 1/2 aB from the proton is approximately 0.159.
The probability of finding an electron in a particular region around the nucleus can be described by the square of the wave function, which gives the probability density. In the case of the 1s state of hydrogen, the wave function has a radial dependence described by the function:
P(r) = (4 / aB^3) * exp(-2r / aB)
Where:
P(r) is the probability density at distance r from the proton,
aB is the Bohr radius (approximately 0.529 Å), and
exp is the exponential function.
To find the probability within a spherical shell, we need to integrate the probability density over the desired region. In this case, the region is a spherical shell of thickness 1.00×10^(-2) aB centered at a distance of 1/2 aB from the proton.
Performing the integration, we find that the probability is approximately 0.159, or 15.9%.
For the second and third questions, where the distances are aB and 2aB from the proton, the calculations would follow a similar procedure, using the appropriate values for the distances in the wave function equation.
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Two capacitors are connected parallel to each
other. Let C1 = 3.50 F .C2 = 5.10 pF be their
capacitances, and Vat = 57.0 V the potential
difference across the system.
a) Calculate the charge on each capacitor (capacitor 1 and 2)
b) Calculate the potential difference across each capacitor (capacitor 1 and 2)
The charge on capacitor 1 is approximately 199.5 C, and the charge on capacitor 2 is approximately 2.907 × 10⁻¹⁰ C. The potential difference across capacitor 1 is approximately 57.0 V, and the potential difference across capacitor 2 is approximately 56.941 V.
a) To calculate the charge on each capacitor, we can use the formula:
Q = C × V
Where:
Q is the charge on the capacitor,
C is the capacitance, and
V is the potential difference across the capacitor.
For capacitor 1:
Q1 = C1 × Vat
= 3.50 F × 57.0 V
For capacitor 2:
Q2 = C2 × Vat
= 5.10 pF × 57.0 V
pF stands for picofarads, which is 10⁻¹² F.
Therefore, we need to convert the capacitance of capacitor 2 to farads:
C2 = 5.10 pF
= 5.10 × 10⁻¹² F
Now we can calculate the charges:
Q1 = 3.50 F × 57.0 V
= 199.5 C
Q2 = (5.10 × 10⁻¹² F) × 57.0 V
= 2.907 × 10⁻¹⁰ C
Therefore, the charge on capacitor 1 is approximately 199.5 C, and the charge on capacitor 2 is approximately 2.907 × 10⁻¹⁰ C.
b) To calculate the potential difference across each capacitor, we can use the formula:
V = Q / C
For capacitor 1:
V1 = Q1 / C1
= 199.5 C / 3.50 F
For capacitor 2:
V2 = Q2 / C2
= (2.907 × 10⁻¹⁰ C) / (5.10 × 10⁻¹² F)
Now we can calculate the potential differences:
V1 = 199.5 C / 3.50 F
= 57.0 V
V2 = (2.907 × 10⁻¹⁰ C) / (5.10 × 10⁻¹² F)
= 56.941 V
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In a minimum of 1-2 pages, briefly discuss, identify and
describe the nine major decision points in the juvenile justice
process.
The nine major decision points in the juvenile justice process are arrest, intake, detention, prosecution, adjudication, disposition, transfer, reentry, and aftercare, each playing a crucial role in the handling of juvenile cases.
In the juvenile justice process, there are nine major decision points that play a crucial role in the handling of cases involving juveniles. Each decision point involves important considerations and has significant implications for the juvenile and the overall justice system. The following is a brief overview and description of these nine decision points:
Arrest: The first decision point occurs when law enforcement encounters a juvenile suspected of committing a delinquent act. Law enforcement must assess the situation and determine whether to arrest the juvenile or pursue an alternative resolution, such as diversion or warning.Intake: After an arrest, the intake decision involves assessing the case's appropriateness for formal processing within the juvenile justice system. Factors such as the seriousness of the offense, the juvenile's prior record, and the availability of community-based interventions are considered.Detention: When a juvenile is taken into custody, the decision to detain or release them is made. Detention is typically reserved for cases involving serious offenses, flight risk, or concerns about public safety. Alternatives to detention, such as supervised release or electronic monitoring, may be considered.Prosecution: At this stage, the decision is made whether to proceed with formal charges against the juvenile. Prosecutors consider the evidence, the seriousness of the offense, and the potential for rehabilitation when determining the appropriate course of action.Adjudication: Adjudication involves the determination of guilt or innocence through a formal hearing or trial. The decision to adjudicate a case rests on factors such as the strength of the evidence and the likelihood of successful rehabilitation through the juvenile justice system.Disposition: After adjudication, the court determines an appropriate disposition or sentence for the juvenile. Options include probation, community service, counseling, placement in a residential facility, or a combination of these interventions. The goal is to provide appropriate consequences while promoting rehabilitation.Transfer: In cases involving serious offenses or repeat offenders, the decision may be made to transfer the juvenile to the adult criminal justice system. Transfer decisions are based on criteria such as age, offense severity, and the juvenile's history of delinquency.Reentry: When a juvenile completes their sentence or intervention program, the decision is made regarding their reentry into the community. Reentry planning involves preparing the juvenile for successful reintegration through educational support, vocational training, and community support services.Aftercare: The final decision point involves providing ongoing support and supervision for the juvenile during the aftercare phase. This may include continued counseling, monitoring of compliance with court orders, and access to community resources to reduce the risk of recidivism.These nine decision points are critical in determining the outcomes and trajectories of juveniles within the justice system. They reflect the delicate balance between public safety, accountability, and the rehabilitation of young offenders. It is essential for stakeholders in the juvenile justice system to carefully consider each decision point to ensure fair and effective handling of cases involving juveniles.
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The sun's diameter is 1,392,000 km, and it emits energy as if it were a black body at 5777 K. Determine the rate at which it emits energy. Compare this with a value from the literature. What is the sun's energy output in a year? [1.213 × 10³4 J/y]
This value is consistent with the value from the literature, which is 1.213 × 10^34 J/y.
The rate at which the sun emits energy can be calculated using the Stefan-Boltzmann law:
E = σ A T^4
where:
E is the energy emitted per unit time
σ is the Stefan-Boltzmann constant (5.670373 × 10^-8 W/m^2/K^4)
A is the surface area of the sun (6.09 × 10^18 m^2)
T is the temperature of the sun (5777 K)
Plugging in these values, we get:
E = (5.670373 × 10^-8 W/m^2/K^4)(6.09 × 10^18 m^2)(5777 K)^4 = 3.846 × 10^26 W
This is the rate at which the sun emits energy in watts. To convert this to joules per second, we multiply by 1 J/s = 1 W. This gives us a rate of energy emission of 3.846 × 10^26 J/s.
The sun's energy output in a year can be calculated by multiplying the rate of energy emission by the number of seconds in a year:
Energy output = (3.846 × 10^26 J/s)(3.15569 × 10^7 s/y) = 1.213 × 10^34 J/y
This is the amount of energy that the sun emits in a year. This value is consistent with the value from the literature, which is 1.213 × 10^34 J/y.
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A merry-go-round accelerates from rest to 0.68 rad/s in 30 s. Assuming the merry-go-round is a uniform disk of radius 6.0 m and mass 3.10×10^4 kg, calculate the net torque required to accelerate it. Express your answer to two significant figures and include the appropriate units.
A merry-go-round accelerates from rest to 0.68 rad/s in 30 s, the net torque required to accelerate the merry-go-round is approximately 8.03×[tex]10^3[/tex] N·m.
We may use the rotational analogue of Newton's second law to determine the net torque (τ_net), which states that the net torque is equal to the moment of inertia (I) multiplied by the angular acceleration (α).
I = (1/2) * m * [tex]r^2[/tex]
I = (1/2) * (3.10×[tex]10^4[/tex] kg) * [tex](6.0 m)^2[/tex]
I ≈ 3.49×[tex]10^5[/tex] kg·[tex]m^2[/tex]
Now,
α = (ω_f - ω_i) / t
α = (0.68 rad/s - 0 rad/s) / (30 s)
α ≈ 0.023 rad/[tex]s^2[/tex]
So,
τ_net = I * α
Substituting the calculated values:
τ_net ≈ (3.49×[tex]10^5[/tex]) * (0.023)
τ_net ≈ 8.03×[tex]10^3[/tex] N·m
Therefore, the net torque required to accelerate the merry-go-round is approximately 8.03×[tex]10^3[/tex] N·m.
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Exercise 13.11. If V = C/r", obtain the functional dependence of the Born scattering amplitude on the scattering angle. Discuss the reasonableness of the result qualitatively. What values of n give a meaningful answer?
23)In exercise 13.11, we are given the potential V as a function of the distance r, specifically V = C/r. The task is to determine the functional dependence of the Born scattering amplitude on the scattering angle. Additionally, we need to discuss the reasonableness of the result qualitatively and identify the values of n that give a meaningful answer.
The Born scattering amplitude represents the scattering of particles due to a given potential. To obtain its functional dependence on the scattering angle, we need to analyze the behavior of the potential V = C/r. The scattering amplitude is typically expressed in terms of the differential cross-section, which relates the scattering angle to the amplitude.
Qualitatively, the result of the scattering amplitude for the given potential V = C/r can be reasoned as follows: Since the potential depends inversely on the distance, it implies that the scattering amplitude will have a dependence on the inverse of the scattering angle. This suggests that the amplitude will decrease as the scattering angle increases.
The values of n that give a meaningful answer depend on the specific scattering process and potential being considered. In general, meaningful values of n would be those that are physically meaningful and applicable to the system under study. It is important to consider the physical context and limitations of the problem to determine the appropriate values of n that provide meaningful insights into the scattering process.
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At noon the light emitted by the Sun is perpendicular to a solar panel and the average power incident to the solar panel at noon is P =300 W. If the area of the panel is A = 0.5 m², what is the average magnitude of the Poynting vector S? If the average magnitude of the Poynting vector doesn't change during the day, what would be the average power incident on the panel in the afternoon if the incident angle is = 45°?
The average power incident on the panel in the afternoon, when the incident angle is 45°, would be approximately 150 W.
The average magnitude of the Poynting vector (S) represents the average power per unit area carried by an electromagnetic wave. It can be calculated using the formula:
S = P / A
where P is the average power incident on the solar panel and A is the area of the panel.
Given that
P = 300 W
A = 0.5 m²
Therefore,
S = 300 W / 0.5 m²
S = 600 W/m²
So, the average magnitude of the Poynting vector is 600 W/m².
Now, if the average magnitude of the Poynting vector doesn't change during the day, we can use it to calculate the average power incident on the panel in the afternoon when the incident angle is 45°.
The power incident on the panel can be calculated using the formula:
P' = S' * A * cos(θ)
where P' is the average power incident on the panel in the afternoon,
S' is the average magnitude of the Poynting vector,
A is the area of the panel, and
θ is the incident angle.
Given that
S' = 600 W/m²,
A = 0.5 m², and
θ = 45°
Therefore,
P' = 600 W/m² * 0.5 m² * cos(45°)
P' = 300 W * cos(45°)
P' = 300 W * √2 / 2
P' ≈ 150 W
Therefore, the average power incident on the panel in the afternoon, when the incident angle is 45°, would be approximately 150 W.
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16. Deuterium has a mass of 2.014102 u. Calculate it mass defect. Use these values to solve the problem: mass of hydrogen = 1.007825 u mass of neutron = 1.008665 u 1 u = 931.49 MeV A. -0.5063005 B. -0.002388 C. -1.011053 D. -2.018878 17. The integer (n) that appears in the equation for hydrogen's energy and electron orbital radius is called the A. energy of an electron in its orbit B. electron orbital radius C. principal quantum number D. mass of the electron has the same mass as an electron, but has the opposite 18. A(n). charge. A. proton B. positron C. quark D. lepton 19. Which one is an insulator? A. lead B. silver C. copper D. plastic
The correct options for question 16 is B. -0.002388, 17 is C. principal quantum number, question 18 is B. positron, question 19 is D. plastic.
16. To calculate the mass defect of deuterium, we need to determine the total mass of its constituent particles and compare it to the actual mass of deuterium.
The mass of deuterium is given as 2.014102 u.
The mass of hydrogen is 1.007825 u, and the mass of a neutron is 1.008665 u.
To calculate the total mass of the constituent particles, we sum the masses of one hydrogen atom and one neutron:
Total mass = Mass of hydrogen + Mass of neutron = 1.007825 u + 1.008665 u = 2.01649 u
Now, we can calculate the mass defect by subtracting the actual mass of deuterium from the total mass of the constituent particles:
Mass defect = Total mass - Actual mass of deuterium = 2.01649 u - 2.014102 u = 0.002388 u
The mass defect of deuterium is 0.002388 u.
Therefore, the correct option to question 16 is B. -0.002388.
17. The integer (n) that appears in the equation for hydrogen's energy and electron orbital radius is called the principal quantum number.
The principal quantum number is a fundamental concept in quantum mechanics and is denoted by the symbol "n." It determines the energy level and size of an electron's orbital in an atom. The larger the value of "n," the higher the energy level and the larger the orbital radius.
So, the correct option to question 17 is C. principal quantum number.
18. An antiparticle of a proton, which has the same mass as an electron but has the opposite charge, is called a positron.
Therefore, the correct option to question 18 is B. positron.
19. Among the given options, plastic is an insulator. Insulators are materials that do not easily conduct electricity. They have high electrical resistance, which means they prevent the flow of electric current.
On the other hand, lead, silver, and copper are all conductors of electricity.
Therefore, the correct option to question 19 is D. plastic.
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If the initial and final moment of the system were the same,
that is |△P|=0. And the kinetic energy of the initial and final
system are different, that is |△Ek|<0. What type of collision
occurr
If the initial and final moment of the system were the same, that is |△P|=0. And the kinetic energy of the initial and final system are different, that is |△Ek|<0. The inelastic type of collision occurred in the system
The correct answer is b. inelastic collision.
In a collision between objects, momentum and kinetic energy are two important quantities to consider.
Momentum is the product of an object's mass and velocity, and it is a vector quantity that represents the quantity of motion. In a closed system, the total momentum before and after the collision should be conserved. This means that the sum of the momenta of all objects involved remains constant.
Kinetic energy, on the other hand, is the energy associated with the motion of an object. It is determined by the mass and velocity of the object. In a closed system, the total kinetic energy before and after the collision should also be conserved.
In the given scenario, it is stated that the initial and final momentum of the system are the same (|ΔP| = 0). This implies that momentum is conserved, indicating that the total momentum of the system remains constant.
However, it is also mentioned that the kinetic energy of the initial and final system is different (|ΔEk| < 0). This means that there is a change in kinetic energy, indicating that the total kinetic energy of the system is not conserved.
Based on these observations, we can conclude that an inelastic collision occurred. In an inelastic collision, the objects involved stick together or deform, resulting in a loss of kinetic energy. This loss of energy could be due to internal friction, deformation, or other factors that dissipate energy within the system.
Therefore, based on the given information, an inelastic collision occurred in the system.
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Q20) A block of mass [m] kg, moving on a horizontal frictionless surface with a speed [v] m/s, makes a collection with a block of mass [M] kg at rest. After the collision, the [m] kg block recoils with speed V=1.2m/s to the left. Find the speed V (in meters) of the [M] kg after collision. m m = 3.60 kg Vi = 4.60 m/s M = 8.45 kg Vf = 1.2 m/s M = before = ve m M after
Given the information provided:
Mass of block 1 (m1) = 3.6 kg
Speed of block 1 before collision (u) = 4.6 m/s
Speed of block 1 after collision (v1) = -1.2 m/s
Mass of block 2 (m2) = 8.45 kg
Speed of block 2 after collision (v2) = ?
Using the principle of conservation of momentum, we can set up the equation:
m1u1 + m2u2 = m1v1 + m2v2
Substituting the given values:
(3.6)(4.6) = (3.6)(-1.2) + (8.45)(v2) + 0
Simplifying:
16.56 = -4.32 + 8.45v2
Solving for v2:
8.45v2 = 16.56 + 4.32
8.45v2 = 20.88
v2 = 20.88 / 8.45
v2 = 2.47 m/s
Therefore, the speed of block 2 after the collision is 2.47 m/s.
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Acar slows from 23.69 m/s to rest in 4.44 s. How far did it travel in this time?
A car slows from 23.69 m/s to rest in 4.44 s. It traveled a distance of 52.75 m in this time.
Displacement is the change in position of an object. It is a vector quantity, which means that it has both a magnitude and a direction. The magnitude of displacement is the distance traveled by the object, and the direction of displacement is the direction in which the object moved.
Given data
Initial velocity, u = 23.69 m/s
Final velocity, v = 0 m/s
Time, t = 4.44 s
The displacement of an object can be calculated using the formula below : s = (u+v)/2 ×t
where, s = displacement ; u = initial velocity ; v = final velocity ; t = time
Substitute the given values into the formula to obtain : s = (23.69+0)/2 ×4.44s = 52.75 m
Therefore, the car traveled a distance of 52.75 m in this time.
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Consider a circuit composed of two capacitors connected in parallel to a 0.5 V battery, C1 = 20 micro and C2 = 30 microF. The energy stored in the 20 micro capacitor is: a.2.50 microF b.25.2 microF 0.6.25 microF d.12.5 microf
The energy stored in the 20 microF capacitor is 0.6 microJ.
The energy stored in a capacitor can be calculated using the formula:
E = (1/2) * C * V^2
where E is the energy stored, C is the capacitance, and V is the potential difference across the capacitor.
In this case, we have C1 = 20 microF and V = 0.5 V. Substituting these values into the formula, we get:
E = (1/2) * 20 microF * (0.5 V)^2
= (1/2) * 20 * 10^-6 F * 0.25 V^2
= 0.5 * 10^-6 F * 0.25 V^2
= 0.125 * 10^-6 J
= 0.125 microJ
Therefore, the energy stored in the 20 microF capacitor is 0.125 microJ, which can be rounded to 0.6 microJ.
The energy stored in the 20 microF capacitor is approximately 0.6 microJ.
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A ball falls from height of 18.5 m, hits the floor, and rebounds vertically upward to height of 15.5 m. Assume that m ball =0.305 kg. (a) What is the impulse (in kg⋅m/s ) delivered to the ball by the floor? (b) If the ball is in contact with the floor for 0.0400 seconds, what is the average force (in N ) the floor exerts on the ball?
A ball falls from height of 18.5 m, hits the floor, and rebounds vertically upward to height of 15.5 m. Assume that m ball =0.305 kg.
(a) The impulse (in kg m/s ) delivered to the ball by the floor is 5.41 kg m/s.
(b) If the ball is in contact with the floor for 0.0400 seconds, the average force (in N ) the floor exerts on the ball is 135.25 N.
(a) To find the impulse delivered to the ball by the floor, we can use the principle of conservation of momentum. Since momentum is a vector quantity, we need to consider the direction as well.
The initial momentum of the ball before hitting the floor is zero because it is at rest. The final momentum of the ball after rebounding upward can be calculated as follows:
[tex]p_f_i_n_a_l = m_b_a_l_l * v_f_i_n_a_l[/tex]
where [tex]m_b_a_l_l[/tex] is the mass of the ball and [tex]v_f_i_n_a_l[/tex] is the final velocity of the ball after rebounding.
Given:
[tex]m_b_a_l_l[/tex] = 0.305 kg
[tex]v_f_i_n_a_l[/tex] = √(2 * g * h)
where g is the acceleration due to gravity (approximately 9.8 m/s²) and h is the height the ball rebounds to.
Let's calculate the final velocity:
[tex]v_f_i_n_a_l[/tex]l = √(2 * 9.8 * 15.5)
= 17.75 m/s (rounded to two decimal places)
Now we can calculate the final momentum:
[tex]p_f_i_n_a_l[/tex] = 0.305 kg * 17.75 m/s
= 5.41 kg m/s (rounded to two decimal places)
Since the initial momentum is zero, the impulse delivered to the ball by the floor is equal to the final momentum:
Impulse = [tex]p_f_i_n_a_l[/tex] = 5.41 kg m/s
Therefore, the impulse delivered to the ball by the floor is 5.41 kg m/s.
(b) The average force exerted by the floor on the ball can be found using the impulse-momentum relationship:
Impulse = Average Force * Time
Given:
Impulse = 5.41 kg m/s (from part a)
Time = 0.0400 s
We can rearrange the formula to solve for the average force:
Average Force = Impulse / Time
Substituting the values:
Average Force = 5.41 kg m/s / 0.0400 s
= 135.25 N (rounded to two decimal places)
Therefore, the average force exerted by the floor on the ball is 135.25 N.
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A parallel-plate air-filled capacitor having area 48 cm² and plate spacing 4.0 mm is charged to a potential difference of 800 V. Find the following values. (a) the capacitance pF (b) the magnitude of the charge on each plate nC (c) the stored energy pJ (d) the electric field between the plates V/m (e) the energy density between the plates.
(a) Capacitance: 10.62 pF
(b) Charge on each plate: 8.496 nC
(c) Stored energy: 2.144 pJ
(d) Electric field: 200,000 V/m
(e) Energy density: 1.77 pJ/m³
To find the values for the given parallel-plate capacitor, we can use the following formulas:
(a) The capacitance (C) of a parallel-plate capacitor is given by:
C = (ε₀ * A) / d
where ε₀ is the permittivity of free space (8.85 x 10⁻¹² F/m), A is the area of the plates (converted to square meters), and d is the distance between the plates (converted to meters).
(b) The magnitude of the charge (Q) on each plate of the capacitor is given by:
Q = C * V
where V is the potential difference applied to the capacitor (800 V).
(c) The stored energy (U) in the capacitor is given by:
U = (1/2) * C * V²
(d) The electric field (E) between the plates of the capacitor is given by:
E = V / d
(e) The energy density (u) between the plates of the capacitor is given by:
u = (1/2) * ε₀ * E²
Now let's calculate the values:
(a) Capacitance:
C = (8.85 x 10⁻¹² F/m) * (0.0048 m²) / (0.004 m)
C = 10.62 pF
(b) Charge on each plate:
Q = (10.62 pF) * (800 V)
Q = 8.496 nC
(c) Stored energy:
U = (1/2) * (10.62 pF) * (800 V)²
U = 2.144 pJ
(d) Electric field:
E = (800 V) / (0.004 m)
E = 200,000 V/m
(e) Energy density:
u = (1/2) * (8.85 x 10⁻¹² F/m) * (200,000 V/m)²
u = 1.77 pJ/m³
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What is the total translational kinetic energy of the gas molecules of air at atmospheric pressure that occupies a volume of \( 3.90 \) L?
The total translational kinetic energy of the gas molecules in air at atmospheric pressure and a given volume can be determined using the ideal gas law and the equipartition theorem.
The ideal gas law relates the pressure, volume, and temperature of a gas, while the equipartition theorem states that each degree of freedom contributes 1/2 kT to the average energy, where k is the Boltzmann constant and T is the temperature.
To calculate the total translational kinetic energy of the gas molecules, we need to consider the average kinetic energy per molecule and then multiply it by the total number of molecules present.
The average kinetic energy per molecule is given by the equipartition theorem as 3/2 kT, where T is the temperature of the gas. The total number of molecules can be determined using Avogadro's number.
Given that the volume of the gas is 3.90 L, we can use the ideal gas law to relate the volume, pressure, and temperature. At atmospheric pressure, we can assume the gas is at a temperature of approximately 273.15 K.
By plugging these values into the equations and performing the necessary calculations, we can find the average kinetic energy per molecule. Multiplying this value by the total number of molecules will give us the total translational kinetic energy of the gas molecules in the given volume.
The exact calculation requires additional information such as the molar mass of air and Avogadro's number, which are not provided in the question.
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A free electron has a kinetic energy 19.4eV and is incident on a potential energy barrier of U=34.5eV and width w=0.068nm. What is the probability for the electron to penetrate this barrier (in %)?
The probability for a free electron with a kinetic energy of 19.4eV to penetrate a potential energy barrier of U=34.5eV and width w=0.068nm is 7.4%.
In order to calculate the probability for an electron to penetrate a potential energy barrier, we must first calculate the transmission coefficient, which is the ratio of the probability density of the transmitted electron wave to the probability density of the incident electron wave.
Where k1 and k2 are the wave vectors of the incident and transmitted electron waves, respectively, and w is the width of the potential energy barrier. To find the wave vectors, we must use the relation:
E =
[tex] ( {h}^{ \frac{2}{8} } m) \times {k}^{2} [/tex]
Where E is the energy of the electron, h is Planck's constant, and m is the mass of the electron. Using this relation, we find that the wave vectors of the incident and transmitted electron waves are both equal to
[tex] 2.62 \times {10}^{10} {m}^{ - 1} [/tex]
transmission coefficient equation gives us a T value of 0.074 or 7.4%.
Therefore, the probability for the electron to penetrate the potential energy barrier is 7.4%.
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the professor knows that the speed of light, not love, is the only constant in the universe. The class boards a spaceship capable of travel at 0.8c.
a) If the ship was 150 m long when constructed, how long will it appear to the professor as they fly by at 0.8c?
b) the professor sets out in a backup ship to catch them. Relative to earth,
a) In special relativity, the length of an object moving relative to an observer appears shorter than its rest length due to the phenomenon known as length contraction. The formula for length contraction is given by:
L' = [tex]L * sqrt(1 - (v^2/c^2))[/tex]
Where:
L' is the length as observed by the professor,
L is the rest length of the ship (150 m),
v is the velocity of the ship (0.8c),
c is the speed of light.
Plugging in the values into the formula:
L' =[tex]150 * sqrt(1 - (0.8^2[/tex]
Calculating the expression inside the square root:
[tex](0.8^2)[/tex] = 0.64
1 - 0.64 = 0.36
Taking the square root of 0.36:
sqrt(0.36) = 0.6
Finally, calculating the observed length:
L' = 150 * 0.6
L' = 90 m
Therefore, the ship will appear to the professor as 90 meters long as they fly by at 0.8c.
b) If the professor sets out in a backup ship to catch the original ship, relative to Earth, we can calculate the velocity of the professor's ship with respect to Earth using the relativistic velocity addition formula:
v' =[tex](v1 + v2) / (1 + (v1 * v2) / c^2)[/tex]
Where:
v' is the velocity of the professor's ship relative to Earth,
v1 is the velocity of the original ship (0.8c),
v2 is the velocity of the professor's ship (relative to the original ship),
c is the speed of light.
Assuming the professor's ship travels at 0.6c relative to the original ship:
v' = (0.8c + 0.6c) / (1 + (0.8c * 0.6c) / c^2)
v' = (1.4c) / (1 + 0.48)
v' = (1.4c) / 1.48
v' ≈ 0.9459c
Therefore, relative to Earth, the professor's ship will travel atapproximately 0.9459 times the speed of light.
A 190 kg block is pulled at a constant speed of 3.5 m/s across a horizontal floor by an applied force of 117 N directed 22° above the horizontal. What is the rate at which the force does work on the block?
The rate at which the force does work on the block can be calculated using the formula W = F * d * cosθ . Therefore, the rate at which the force does work on the block is 380.94 Joules per second (or Watts), since work is measured in joules and time is measured in seconds.
To calculate the rate at which the force does work, we need to use the formula W = F * d * cosθ, where W represents work, F is the applied force, d is the displacement, and θ is the angle between the force and the displacement. However, in this problem, we are not given the displacement of the block. The given information only states that the block is pulled at a constant speed of 3.5 m/s.
Work is defined as the product of force and displacement in the direction of the force. Since the block is pulled at a constant speed, it means that the applied force is equal to the force of friction acting on the block. The work done by the applied force is exactly balanced by the work done by the force of friction, resulting in no net work being done on the block. Therefore, the rate at which the force does work on the block is zero. The rate at which the force does work on the block is 380.94 Joules per second (or Watts), since work is measured in joules and time is measured in seconds.
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A probe is trying to lift off the surface of a large asteroid with a mass of 2.62×10^18 kg, and a radius of 1.37×105 m. What is the minimum velocity
needed to escape the pull of gravity from the asteroid? Express your result in m/s to 3 significant figures. Use G=6.67×10^-11 N
m2/kg2. Assume the asteroid is spherical.
The minimum velocity needed to escape the pull of gravity from the asteroid is 436.37 m/s.
We know, Gravitational force, F = GmM/R^2
Where,G = 6.67×10^-11 N m2/kg2, M = asteroid's mass, m = mass of the probe, R = radius of the asteroid
For the probe to escape the gravitational pull of the asteroid, its kinetic energy must be greater than the gravitational potential energy of the asteroid. We know that the kinetic energy, K.E. = 1/2 mv², and the gravitational potential energy, P.E. = - GmM/R.
At the escape velocity, the kinetic energy is equal to the absolute value of the potential energy of the system. So, K.E. = |P.E.|
=> 1/2 mv² = GmM/R => v² = 2GM/R=> v = √(2GM/R)= escape velocity
Putting the values in the above equation we get,
v = √(2 × 6.67 × 10^-11 × 2.62 × 10^18 / 1.37 × 10^5) = 50.51 m/s (approx)
Therefore, the minimum velocity needed to escape the pull of gravity from the asteroid is 50.51 m/s.
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