Self-Assessment Quiz: Newton's Laws in Space
Twenty questions on Newton's laws, momentum, gravitation, and escape velocity. Answer each before opening the key. Aim for 16 or more. Use $\mu_\oplus = 3.986\times10^{5}\ \text{km}^3/\text{s}^2$ and $R_\oplus = 6{,}371\ \text{km}$ where needed.
Question 1
Newton's first law explains why, in the vacuum of space, a coasting spacecraft:
A) gradually slows down and stops B) keeps moving at constant velocity with no fuel C) needs continuous thrust to maintain speed D) speeds up on its own
Question 2
A satellite in a high, stable orbit runs out of fuel. It will:
A) immediately fall to Earth B) slow down and drift away C) continue orbiting essentially indefinitely D) stop moving
Question 3
An orbit persists (in a vacuum) because:
A) the spacecraft's engine constantly fights gravity B) there is no gravity in orbit C) inertia supplies sideways motion while gravity bends it into a closed loop, with no friction to remove energy D) the spacecraft is beyond Earth's reach
Question 4
In its most general form, Newton's second law is best written:
A) $F = ma$ B) $F = mv$ C) $F = dp/dt$ D) $F = \mu/r^2$
Question 5
Why must a rocket be described by the momentum form of the second law rather than simply $F = ma$?
A) rockets move too fast for $F = ma$ B) a rocket's mass changes as it burns propellant C) gravity is stronger in space D) $F = ma$ only works on Earth
Question 6
The thrust of a rocket is given by:
A) $T = \dot m_p / v_e$ B) $T = \dot m_p\, v_e$ C) $T = v_e / \dot m_p$ D) $T = m\,v_e$
Question 7
In a vacuum, the only way for a spacecraft to change its velocity is to:
A) push against the surrounding space B) push against sunlight C) throw mass in the opposite direction D) use a propeller
Question 8
A rocket works in vacuum because it pushes against:
A) the air B) its own expelled propellant C) the launch pad D) Earth's magnetic field
Question 9
Conservation of momentum states that, with no external force, the total momentum of a system:
A) always increases B) always decreases C) stays constant D) equals zero
Question 10
Conservation of momentum is most directly a consequence of Newton's:
A) first law B) second law C) third law D) law of gravitation
Question 11
The gravitational parameter $\mu$ of a body is defined as:
A) $G/M$ B) $GM$ C) $M/G$ D) $g_0 R$
Question 12
The acceleration gravity gives a falling spacecraft is $a = \mu/r^2$, which does not depend on the spacecraft's own mass because:
A) spacecraft are very light B) the mass cancels: gravitational force is proportional to $m$, and $a = F/m$ C) space has no gravity D) $\mu$ already includes the spacecraft's mass
Question 13
Escape velocity from a body of gravitational parameter $\mu$ and radius $R$ is:
A) $\sqrt{\mu/R}$ B) $\sqrt{2\mu/R}$ C) $2\mu/R$ D) $\mu/R^2$
Question 14
Earth's escape velocity from the surface is about:
A) $7.8\ \text{km/s}$ B) $9.4\ \text{km/s}$ C) $11.2\ \text{km/s}$ D) $25\ \text{km/s}$
Question 15
Escape velocity is related to the circular orbital velocity at the same radius by a factor of:
A) $2$ B) $\sqrt{2}$ C) $1/2$ D) $\pi$
Question 16 (True/False, justify)
"There is no gravity at the International Space Station, which is why the astronauts float." True or false? Justify with the approximate value of $g$ there.
Question 17 (True/False, justify)
"A heavier spacecraft needs a higher speed to escape a planet than a lighter one." True or false? Explain in one sentence.
Question 18 (True/False, justify)
"A rocket with more thrust standing on the pad is producing that thrust by pushing on the ground." True or false? Say what it actually pushes on.
Question 19 (Short answer)
An engine expels $250\ \text{kg/s}$ of propellant at an effective exhaust velocity of $3{,}000\ \text{m/s}$. Compute the thrust, showing units.
Question 20 (Short answer)
In one or two sentences, explain why the weightlessness experienced in orbit is called "free fall" rather than "the absence of gravity," and connect it to why an orbit does not decay in vacuum.
Answer Key
| Q | Ans | Note |
|---|---|---|
| 1 | B | Inertia: with no force to stop it, motion persists; fuel only changes motion. |
| 2 | C | In a high orbit, drag is negligible; inertia + gravity maintain the orbit without fuel. |
| 3 | C | Sideways inertia bent into a closed loop by gravity, with no friction to dissipate energy. |
| 4 | C | $F = dp/dt$; it reduces to $F = ma$ only for constant mass. |
| 5 | B | A rocket sheds mass as exhaust, so $m$ is not constant and $F = ma$ is insufficient. |
| 6 | B | $T = \dot m_p v_e$ — mass flow rate times exhaust velocity. |
| 7 | C | Throw mass one way; recoil the other. There is nothing external to push on. |
| 8 | B | It reacts against its own exhaust — which is why it works better in vacuum. |
| 9 | C | With no external force, total momentum is conserved (constant), whatever its value. |
| 10 | C | The third law (equal-opposite internal forces) makes the internal momentum changes cancel. |
| 11 | B | $\mu = GM$, the body's mass folded together with the gravitational constant. |
| 12 | B | $F \propto m$ and $a = F/m$, so $m$ cancels; all objects fall at the same rate. |
| 13 | B | $v_{\text{esc}} = \sqrt{2\mu/R}$, from setting total energy to zero. |
| 14 | C | $\sqrt{2\mu_\oplus/R_\oplus} \approx 11.2\ \text{km/s}$. |
| 15 | B | $v_{\text{esc}} = \sqrt{2}\,v_{\text{circ}}$ at any radius — about 41% more. |
| 16 | False | $g \approx 8.6\ \text{m/s}^2$ at the ISS (~88% of surface); they float because they are in free fall, not because gravity is absent. |
| 17 | False | Escape velocity is independent of the escaping object's mass; $m$ cancels from the energy balance. |
| 18 | False | On the pad it still reacts against its own expelled exhaust; the ground merely supports its weight before liftoff. |
| 19 | — | $T = \dot m_p v_e = 250\ \text{kg/s} \times 3{,}000\ \text{m/s} = 750{,}000\ \text{N} = 750\ \text{kN}$. |
| 20 | — | Astronauts and their craft fall together under real gravity with nothing pushing back, so they feel weightless; the same absence of a dissipating force (no air) is why the orbit — a perpetual fall — does not decay. |
Topics to review by question
| Questions | Topic | Section |
|---|---|---|
| 1, 2, 3 | First law and why orbits don't decay | §2.1 |
| 4, 5, 6, 19 | Second law and thrust | §2.2 |
| 7, 8, 18 | Third law and vacuum propulsion | §2.3 |
| 9, 10 | Conservation of momentum | §2.4 |
| 11, 12 | Universal gravitation and $\mu = GM$ | §2.5 |
| 13, 14, 15, 17 | Escape velocity | §2.6 |
| 16, 20 | Free fall vs. "no gravity" | §2.1, §2.5 |