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joja [24]
3 years ago
13

A model rocket is fired vertically upward from rest. Its acceleration for the first three seconds is a(t) = 96t, at which time t

he fuel is exhausted and it becomes a freely "falling" body. Nineteen seconds later, the rocket's parachute opens, and the (downward) velocity slows linearly to −16 ft/s in 5 s. The rocket then "floats" to the ground at that rate.
a) Determine the position function s and the velocity function v (for all times t).
b) At what time does the rocket reach its maximum height?

What is that height? (Round your answer to the nearest integer.)

c) At what time does the rocket land? (Round your answer to one decimal place.)
Physics
1 answer:
Talja [164]3 years ago
5 0

Answer:

In kinematics questions we need to separate the question into different parts if the acceleration changes. Here, there are three time intervals where acceleration is different.

1) a(t) = 96t. We can find the velocity function of the rocket by integrating the acceleration function. Then we can integrate again to find the position function.

v(t) = \int{a(t)} \, t = \int {96t} \, dt = 48t^2 + C

'C' is the integration constant. We can find this constant by investigating the initial conditions.

v(t = 0) = 48(0)^2 + C = 0\\C = 0

We know that the rocket is initially at rest, so 'C' should be zero.

s(t) = \int {v(t)} \, dt  = \int {48t^2} \, dt = 16t^3 + C

Again, the rocket started from ground zero, so C = 0.

We should conclude the first part by calculating the final position and final velocity of the rocket.

s(t=3) = 16(3)^3 = 432ft\\v(t=3) = 48(3)^2 = 432ft/s

2) For the second part, the rocket is in free fall, so

a(t) = -32.2ft/s^2\\v(t) = -32.2t + C\\v(t=3) = -32.2*3 + C = 432\\C = 335.4\\v(t) = -32.2t + 335.4\\s(t) = -16.1t^2 + 335.4t + C\\s(t=3) = -16.1(3)^2 + 335.4*3 + C = 432\\C = 432 + 144.9 - 1006.2 = -429.3\\s(t) = -16.1t^2 + 335.4t - 429.3

The maximum height that the rocket reaches is when its velocity is zero.

So,

v(t) = -32.2t + 335.4 = 0\\t = 10.4 s

The maximum height is

s(t=10.4) = -16.1t^2 + 335.4t - 429.3 = -16.1(10.4)^2 + 335.4*10.4 - 429.3 = -1741.3 + 3488.1 - 429.3 = 1318 ~ft

The final positions for the part 2 is

s(t=19) = -16.1(19)^2 + 335.4*19 - 429.3 = -5812.1 + 6372 - 429.3 = 131.2~ft\\v(t=19) = -32.2*19 + 335..4 = -276.4~ft/s

3) With the parachute, the velocity is dropped from -276.4 to 16 in 5 s.

a(t) = \frac{-16 - (-276.4))}{5} = 52ft/s^2\\v(t) = 52t + C\\v(t= 19) = 52*19 + C= -276.4\\988+ C = -276.4\\C = -1264.4\\v(t) = 52t - 1264.4

s(t) = 26t^2 - 1264.4t + C \\s(t=19) = 26(19)^2 - 1264.4*19 + C = 131.2\\9386 - 24023.6 + C = 131.2\\C = 14768.8\\s(t) = 26t^2 - 1264.4t + 14768.8

The rocket lands

s(t) = 26t^2 - 1264.4t + 14768.8 = 0\\t = 29s.

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worty [1.4K]
T = (v-0)/a
t = (45.5)/(9.8)
= 4.64m/s.

hope this helps :)
7 0
3 years ago
In a loop-the-loop ride a car goes around a vertical, circular loop at a constant speed. The car has a mass m = 268 kg and moves
11111nata11111 [884]
Before we go through the questions, we need to calculate and determine some values first.

r = 11.5 m 
<span>m = 280 kg </span>
<span>Centripetal force = m x v^2/r = 280 x (17.1^2/11.5) = 7119.55 N 
</span>
1) What is the magnitude of the normal force on the care when it is at the bottom of the circle. 

<span>Centripetal force + mg = 7119.55 + (280 x 9.8) = 9863.55 N </span>

<span>2) What is the magnitude of the normal force on the car when it is at the side of the circle. </span>

<span>Centripetal force = 7119.55 N </span>


<span>3) What is the magnitude of the normal force on the car when it is at the top of the circle. </span>

<span>Centripetal force - mg = 7119.55 - (280 x 9.8) = 4375.55 N </span>

<span>4) What is the minimum speed of the car so that it stays in contact with the track at the top of the loop. </span>

√<span>(gr) </span>

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7 0
3 years ago
Which idea is associated with Copernicus? Select one: a. The orbits of the planets are circles. b. The orbits of the planets are
Schach [20]

Answer:

d. The earth rotates around the sun

Explanation:

  • Nicolas Copernicus is considered the first person to give the theory of heliocentric, or Sun-centered system of our planetary system.
  • In the heliocentric system, it is considered that the sun is stationary and the earth revolves around the sun.
  • He stated that the sun is at the center of the universe and the earth spins on its axis once daily and revolves around the sun in one year.
  • And today we know it is correct that earth rotates on its own axis and also revolves around the sun.

8 0
3 years ago
Water exits straight down from a faucet with a 1.96-cm diameter at a speed of 0.55 m/s. The volume flow rate of the water as it
d1i1m1o1n [39]

Answer:

Q = 165.95 cm³ / s,  1)    v = \sqrt{0.55^2 + 19.6 y},  2)  v = 2.05 m / s,

3)  d₂ = 1.014 cm

Explanation:

This is a fluid mechanics exercise

1) the continuity equation is

         Q = v A

where Q is the flow rate, A is area and v is the velocity

         

the area of ​​a circle is

        A = π r²

radius and diameter are related

        r = d / 2

substituting

       A = π d²/4

       Q = π/4   v d²

let's reduce the magnitudes

       v = 0.55 m / s = 55 cm / s

let's calculate

       Q = π/4   55   1.96²

       Q = 165.95 cm³ / s

If we focus on a water particle and apply the zimematics equations

        v² = v₀² + 2 g y

where the initial velocity is v₀ = 0.55 m / s

        v = \sqrt{0.55^2 + 2  \ 9.8\  y}

        v = \sqrt{0.55^2 + 19.6 y}

2) ask to calculate the velocity for y = 0.2 m

        v = \sqrt{0.55^2 + 19.6 \ 0.2}

        v = 2.05 m / s

3) We write the continuous equation for this point 2

        Q = v₂ A₂

        A₂ = Q / v₂

let us reduce to the same units of the SI system

        Q = 165.95 cm³ s (1 m / 10² cm) ³ = 165.95 10⁻⁶ m³ / s

        A₂ = 165.95 10⁻⁶ / 2.05

        A₂ = 80,759 10⁻⁶ m²

area is

        A₂ = π/4   d₂²

        d₂ = \sqrt{4  A_2 / \pi }

        d₂ = \sqrt{ \frac{4 \ 80.759 \ 10^{-6} }{\pi } }

        d₂ = 10.14 10⁻³ m

        d₂ = 1.014 cm

4 0
3 years ago
The amount of gas that a helicopter uses is directly proportional to the number of hours spent flying. the helicopter flies for
igomit [66]

Answer:

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Explanation:

The amount of gas that a helicopter uses for flying varies directly proportional to the number of hours spent flying.

g ∝ T

where g represents amount of gas and T time of flight.

Then,

\therefore \frac{g_1}{g_2}=\frac{T_1}{T_2}

The helicopter files 4 hours and uses 28 gallons of fuel.

Here, g₁= 28 gallons, T₁=4 hours

g₂=?, T₂=5 hours.

\therefore \frac{g_1}{g_2}=\frac{T_1}{T_2}

\Rightarrow \frac{28}{g_2}=\frac{4}{5}

⇒28×5= g₂×4

⇒ g₂×4=28×5

\Rightarrow g_2=\frac{28\times 5}{4}

\Rightarrow g_2=35 gallons

The helicopter uses 35 gallons to fly for 5 hours.

5 0
3 years ago
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