Question:
(II) A rocket rises vertically, from rest, with an acceleration
of 3.2 m/s² until it runs out of fuel at an
altitude of 775 m. After this point, its
acceleration is that of gravity, downward.
(a) What is the velocity of the rocket when it
runs out of fuel?
(b) How long does it take to reach this point?
(c) What maximum altitude does the rocket reach?
(d) How much time (total) does it take to reach
maximum altitude?
(e) With what velocity does it strike the Earth?
(f) How long (total) is it in the air?
Given
-
Initial velocity:
u = 0 m/s
-
Acceleration during powered ascent:
a₁ = +3.2 m/s²
-
Height when fuel runs out:
h = 775 m
-
Acceleration after fuel runs out:
a₂ = −9.8 m/s²
-
Gravitational acceleration:
g = 9.8 m/s²
-
Initial position:
y₀ = 0 m
Understanding the Two Stages of Motion
The rocket experiences two different stages of motion. We must
treat them separately because the acceleration changes when
the fuel runs out.
Stage 1: Powered Ascent
The rocket starts from rest and accelerates upward at
3.2 m/s² until it reaches 775 m.
a₁ = +3.2 m/s²
Stage 2: After Fuel Runs Out
The rocket continues upward under gravity alone,
slows to zero velocity at its maximum altitude,
and then falls back toward Earth.
a₂ = −9.8 m/s²
(a) Velocity When the Rocket Runs Out of Fuel
During the powered ascent, the rocket starts from rest and
accelerates uniformly through a vertical displacement of 775 m.
We know the initial velocity, acceleration, and displacement.
Therefore, we can use the third equation of motion without
calculating time first.
Method 1: Using the Third Equation of Motion
v² = u² + 2as
Substituting the values:
v² = 0² + 2(3.2)(775)
v² = 6.4 × 775
v² = 4960
Taking the positive square root because the rocket is
moving upward:
v = √4960
v ≈ 70.4 m/s
The positive sign indicates upward motion. The rocket is
moving upward when its fuel runs out.
Answer for (a)
The velocity of the rocket when it runs out of fuel is
+70.4 m/s (upward)
(b) Time Taken to Reach the Fuel Cutoff Point
During the first stage, the rocket starts from rest and
accelerates at 3.2 m/s². We have already calculated its
velocity at the end of this stage.
Method 1: Using the First Equation of Motion
v = u + at
Rearranging:
t = (v − u)/a
Substituting:
t₁ = (70.4 − 0)/3.2
Using the unrounded velocity gives:
t₁ ≈ 22.0 s
Thus, the rocket takes approximately 22.0 seconds to reach
an altitude of 775 m and run out of fuel.
Method 2: Using the Second Equation of Motion
We can independently calculate the same time using the
displacement equation.
s = ut + ½at²
775 = 0(t) + ½(3.2)t²
775 = 1.6t²
t² = 775/1.6
t = √484.375
t₁ ≈ 22.0 s
Answer for (b)
The time taken to reach the fuel cutoff point is
t₁ ≈ 22.0 s
(c) Maximum Altitude Reached by the Rocket
After the fuel runs out, the rocket continues moving upward
because it already has an upward velocity of approximately
70.4 m/s. Gravity acts downward and reduces this velocity
until it becomes zero at the highest point.
We must calculate the additional height gained after the
fuel cutoff and add it to the initial 775 m altitude.
Step 1: Calculate the Additional Height
At the maximum altitude, the final velocity is zero.
Taking the fuel cutoff point as the starting position for
this stage, we use the third equation of motion.
v² = u² + 2as
For this stage:
u = +70.4 m/s, v = 0, a = −9.8 m/s²
0 = u² − 2gs
Rearranging:
s = u²/(2g)
Using the unrounded cutoff velocity:
s = 4960/[2(9.8)]
s = 4960/19.6
s ≈ 253.1 m
Step 2: Calculate the Maximum Altitude
The rocket has already reached 775 m when its fuel runs out.
It rises an additional 253.1 m before stopping momentarily.
H = 775 + 253.1
H ≈ 1028.1 m
The maximum altitude is measured from the Earths surface,
which is taken as the zero-height reference.
Answer for (c)
The maximum altitude reached by the rocket is
H ≈ 1.028 × 10³ m
(d) Total Time to Reach Maximum Altitude
The total ascent time consists of two parts:
-
Time during powered ascent.
-
Additional time after the fuel runs out, while the rocket
continues upward under gravity.
Step 1: Calculate the Additional Ascent Time
During the second stage, the initial velocity is approximately
70.4 m/s and the final velocity at the highest point is zero.
The acceleration is −9.8 m/s².
v = u + at
0 = u − gt
gt = u
t₂ = u/g
Substituting the unrounded velocity:
t₂ = √4960/9.8
t₂ ≈ 7.19 s
Step 2: Calculate the Total Ascent Time
T = t₁ + t₂
T = 22.0 + 7.19
T ≈ 29.2 s
The rocket takes approximately 29.2 seconds from launch to
reach its maximum altitude.
Answer for (d)
T ≈ 29.2 s
(e) Velocity with Which the Rocket Strikes the Earth
After reaching its maximum altitude, the rocket falls freely
under gravity. We can calculate its impact velocity using
the third equation of motion, starting from the highest point.
At the maximum altitude:
-
Initial velocity for the falling stage:
u = 0 m/s
-
Displacement to the ground:
s = −1028.1 m
-
Acceleration:
a = −9.8 m/s²
Method 1: Using the Third Equation of Motion
v² = u² + 2as
Substituting:
v² = 0² + 2(−9.8)(−1028.1)
Using the unrounded maximum altitude:
v² ≈ 20150
Taking the square root:
v ≈ ±142.0 m/s
The positive root would represent upward motion, whereas the
negative root represents downward motion. Since the rocket
is striking the Earth while falling, we choose the negative
root.
Alternative Check: Starting at Fuel Cutoff
We can also calculate the impact velocity directly from
the fuel cutoff point, where the rocket is moving upward
at approximately 70.4 m/s from an altitude of 775 m.
v² = u² + 2as
v² = 4960 + 2(−9.8)(−775)
v² = 4960 + 15190
v² = 20150
v ≈ −142.0 m/s
The negative sign indicates that the rocket is moving
downward when it reaches the ground.
Answer for (e)
Taking upward as positive, the velocity when the rocket
strikes the Earth is
v ≈ −142.0 m/s
Speed of impact ≈ 142.0 m/s, directed downward.
(f) Total Time the Rocket Is in the Air
The total time in the air consists of three intervals:
-
Powered ascent.
-
Additional ascent after the fuel runs out.
-
Descent from the maximum altitude to the ground.
Step 1: Calculate the Time Taken to Fall from Maximum Altitude
From the maximum altitude, the rocket starts falling from rest.
We use the second equation of motion to calculate the falling
time.
s = ut + ½at²
Taking downward as the direction of displacement for this
falling stage:
H = ½gt₃²
Rearranging:
t₃ = √(2H/g)
Substituting H ≈ 1028.1 m:
t₃ = √[2(1028.1)/9.8]
t₃ = √209.8
t₃ ≈ 14.5 s
Step 2: Calculate the Total Time in the Air
The total time is the sum of the powered ascent time,
the additional ascent time, and the falling time.
T_air = t₁ + t₂ + t₃
T_air ≈ 22.0 + 7.19 + 14.5
T_air ≈ 43.7 s
Therefore, the rocket remains in the air for approximately
43.7 seconds from launch until it reaches the Earth.
Answer for (f)
T_air ≈ 43.7 s
Summary of All Six Answers
|
Part
|
Quantity
|
Answer
|
| (a) |
Velocity at fuel cutoff |
+70.4 m/s |
| (b) |
Time to fuel cutoff |
22.0 s |
| (c) |
Maximum altitude |
1028.1 m |
| (d) |
Total time to maximum altitude |
29.2 s |
| (e) |
Impact velocity |
−142.0 m/s |
| (f) |
Total time in the air |
43.7 s |
Key Equations
-
Third equation of motion:
v² = u² + 2as
-
First equation of motion:
v = u + at
-
Second equation of motion:
s = ut + ½at²
-
Additional upward height after fuel cutoff:
h = u²/(2g)
-
Time to maximum altitude after fuel cutoff:
t = u/g
-
Time to fall from maximum altitude:
t = √(2H/g)
Key Idea
When solving a multistage motion problem, calculate the
velocity and time at the transition between stages.
Use the final conditions of one stage as the initial
conditions of the next stage.
Powered ascent → Free ascent → Free fall