Physics ยท Science General
Escape Velocity and Rockets
77 Questions
Escape velocity and rockets questions cover spacecraft trajectories and gravitational influences. The topics include calculating maximum velocities and understanding multistage rocket mechanics. These physics concepts are essential for technical exams requiring scientific aptitude.
Escape velocityOrbital mechanicsRocket propulsionAtmospheric entry speedsGravitational pull
Escape Velocity and Rockets Questions
What is the equation of motion for a spacecraft in a central gravitational field?
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$F = ma$
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$F = GmM/r^2$
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$F = mv^2/r$
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$F = Gm_1m_2/r^2$
B
Correct answer
Explanation
The equation of motion for a spacecraft in a central gravitational field is $F = GmM/r^2$, where $F$ is the gravitational force, $G$ is the gravitational constant, $m$ is the mass of the spacecraft, $M$ is the mass of the central body, and $r$ is the distance between the spacecraft and the central body.
What is the term for the point at which a rocket reaches its maximum altitude?
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Apogee
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Perigee
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Burnout
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Translunar injection
A
Correct answer
Explanation
Apogee is the highest point in a rocket's trajectory.
What is the maximum altitude that the New Shepard rocket can reach?
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100 km
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200 km
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300 km
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400 km
A
Correct answer
Explanation
The New Shepard rocket can reach a maximum altitude of 100 kilometers (62 miles) above Earth's surface.
What is the payload capacity of the New Glenn rocket?
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25,000 kg
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50,000 kg
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75,000 kg
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100,000 kg
B
Correct answer
Explanation
The New Glenn rocket has a payload capacity of 50,000 kilograms (110,000 pounds) to low Earth orbit.
What is the payload capacity of the Electron rocket to low Earth orbit?
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250 kg
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500 kg
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750 kg
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1000 kg
A
Correct answer
Explanation
The Electron rocket has a payload capacity of 250 kg to low Earth orbit.
What is the payload capacity of the Neutron rocket to low Earth orbit?
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2500 kg
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5000 kg
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7500 kg
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10000 kg
Correct answer
Explanation
The Neutron rocket has a payload capacity of 8000 kg to low Earth orbit.
How many stages does the Neutron rocket have?
B
Correct answer
Explanation
The Neutron rocket has two stages.
What was the maximum speed reached by a space shuttle?
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17,500 mph
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25,000 mph
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10,000 mph
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15,000 mph
A
Correct answer
Explanation
The maximum speed reached by a space shuttle was 17,500 mph, which was achieved by the Discovery mission STS-4 in 1982.
What is the term used to describe the process of sending a spacecraft or object out of orbit around a celestial body?
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Ejection
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Extraction
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Escape
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Departure
C
Correct answer
Explanation
Escape is the term used to describe the process of sending a spacecraft or object out of orbit around a celestial body.
What is the recommended ascent rate for scuba diving?
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Ascend at a rate of 10 meters (33 feet) per minute or slower.
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Ascend as quickly as possible to reach the surface.
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Ascend at a rate of 20 meters (66 feet) per minute to avoid decompression sickness.
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Ascend at a rate of 30 meters (98 feet) per minute to save time.
A
Correct answer
Explanation
The recommended ascent rate for scuba diving is 10 meters (33 feet) per minute or slower. This slow ascent rate helps to prevent decompression sickness, which can occur when divers ascend too quickly and nitrogen bubbles form in their bloodstream. Ascending too quickly can also lead to other health problems, such as lung overexpansion injuries.
What is the Tsiolkovsky rocket equation?
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$Delta v = V_e * ln(m_0/m_f)$
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$Delta v = V_e * ln(m_f/m_0)$
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$Delta v = V_e * (m_0/m_f)$
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$Delta v = V_e * (m_f/m_0)$
A
Correct answer
Explanation
The Tsiolkovsky rocket equation is $Delta v = V_e * ln(m_0/m_f)$, where $Delta v$ is the change in velocity, $V_e$ is the effective exhaust velocity, $m_0$ is the initial mass of the rocket, and $m_f$ is the final mass of the rocket.
What is the velocity of a spacecraft at the perigee (closest point) of its elliptical orbit?
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Maximum
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Minimum
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Constant
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Zero
A
Correct answer
Explanation
At the perigee, the spacecraft is closest to the central body and therefore has the highest velocity in its orbit.
A rocket is launched vertically with an initial velocity of 100 m/s. If the rocket's mass is 1000 kg, what is the force acting on the rocket at the moment of launch?
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1000 N
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2000 N
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3000 N
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4000 N
A
Correct answer
Explanation
The force acting on the rocket at the moment of launch is equal to the mass of the rocket multiplied by the acceleration due to gravity (9.8 m/s^2). Since the rocket is moving vertically, the acceleration due to gravity is acting in the opposite direction of the rocket's motion. Therefore, the force acting on the rocket is 1000 kg * 9.8 m/s^2 = 1000 N.
A rocket is launched vertically with an initial velocity of 200 m/s. If the rocket's mass is 2000 kg, what is the force acting on the rocket at the moment of launch?
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2000 N
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4000 N
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6000 N
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8000 N
A
Correct answer
Explanation
The force acting on the rocket at the moment of launch is equal to the mass of the rocket multiplied by the acceleration due to gravity (9.8 m/s^2). Since the rocket is moving vertically, the acceleration due to gravity is acting in the opposite direction of the rocket's motion. Therefore, the force acting on the rocket is 2000 kg * 9.8 m/s^2 = 2000 N.
A rocket is launched vertically with an initial velocity of 300 m/s. If the rocket's mass is 3000 kg, what is the force acting on the rocket at the moment of launch?
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3000 N
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6000 N
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9000 N
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12000 N
A
Correct answer
Explanation
The force acting on the rocket at the moment of launch is equal to the mass of the rocket multiplied by the acceleration due to gravity (9.8 m/s^2). Since the rocket is moving vertically, the acceleration due to gravity is acting in the opposite direction of the rocket's motion. Therefore, the force acting on the rocket is 3000 kg * 9.8 m/s^2 = 3000 N.