Classical-Mechanics Β· Unit 18 Β· Video 1 Β· Interactive Practice

Escape Velocity: Zero Total Energy on Asteroid Toro

IKey Formulas

FormulaNameWhat it says
UG(r)=βˆ’Gmtmr,UG(∞)≑0U^G(r) = -\dfrac{G m_t m}{r}, \qquad U^G(\infty) \equiv 0Gravitational potential energyZero at infinite separation, negative at every finite rr
Kf=0Β atΒ rβ†’βˆžβ€…β€ŠβŸΉβ€…β€ŠEf=0K_f = 0 \text{ at } r \to \infty \;\Longrightarrow\; E_f = 0The escape conditionBarely makes it: nothing left over at infinity
12mvesc2βˆ’GmtmR=0\tfrac{1}{2} m v_{\text{esc}}^2 - \dfrac{G m_t m}{R} = 0Zero mechanical energy at launchWnc=0W_{\text{nc}} = 0, so Ei=Ef=0E_i = E_f = 0
vesc=2GmtRv_{\text{esc}} = \sqrt{\dfrac{2 G m_t}{R}}Escape velocitySet by the asteroid's mtm_t and RR alone

Key Insight: The escaping object's own mass cancels, so a pebble and a person both leave Toro at 7.3Β mβ‹…sβˆ’17.3\ \text{m}\cdot\text{s}^{-1}. What differs is the kinetic energy each must be given: 12mvesc2\tfrac{1}{2}mv_{\text{esc}}^2 still carries the mm.

IIVisualization 1 β€” Three Fates, One Sign

Toro's grip is decided by a sign: whether E=K+UE = K + U at launch is negative, zero, or positive.

IIIVisualization 2 β€” From Ef=0E_f = 0 to 7.3Β m/s7.3\ \text{m/s}

One equation does all the work: the launch kinetic energy exactly fills the well it has to climb out of.

Step 1 β€” The final state fixes the total
Kf=0K_f = 0 at infinite separation is what "escape" means, and Uf=0U_f = 0 is where we put the zero of potential energy.
Ef=Kf+Uf=0E_f = K_f + U_f = 0

IVVisualization 3 β€” How Big Before You Cannot Outrun It?

At Toro's density escape speed grows in proportion to radius, so a bigger rock eventually beats a sprint.

πŸ’‘ Toro's surface gravity is only 5.3Β mmβ‹…sβˆ’25.3\ \text{mm}\cdot\text{s}^{-2}, so a stride that lifts you at 0.15Β mβ‹…sβˆ’10.15\ \text{m}\cdot\text{s}^{-1} leaves you floating for nearly a minute before the next push-off. Reaching 7.3Β mβ‹…sβˆ’17.3\ \text{m}\cdot\text{s}^{-1} is easy on earth; generating it on Toro is the hard part.

VQuiz Questions

Problem 1 Β· Escape Velocity from a Given Body

Given: a uniform spherical asteroid of mass ma=3.0Γ—1015Β kgm_a = 3.0 \times 10^{15}\ \text{kg} and radius R=4.0Γ—103Β mR = 4.0 \times 10^{3}\ \text{m}, with G=6.67Γ—10βˆ’11Β Nβ‹…m2β‹…kgβˆ’2G = 6.67 \times 10^{-11}\ \text{N}\cdot\text{m}^2\cdot\text{kg}^{-2} β€” find the escape velocity from its surface.

βœ… Correct! 2Gma=4.00Γ—105Β m3β‹…sβˆ’22Gm_a = 4.00 \times 10^{5}\ \text{m}^3\cdot\text{s}^{-2}, and dividing by RR gives 100.1Β m2β‹…sβˆ’2100.1\ \text{m}^2\cdot\text{s}^{-2}, whose square root is 10.0Β mβ‹…sβˆ’110.0\ \text{m}\cdot\text{s}^{-1}.
❌ The factor of 2 is missing. Gma/R=7.1\sqrt{Gm_a/R} = 7.1 comes from 12mv2=Gmam/R\tfrac{1}{2}mv^2 = Gm_am/R without multiplying both sides by 22 before taking the root.
❌ That is vesc2v_{\text{esc}}^2, not vescv_{\text{esc}}. 2Gma/R=100.1Β m2β‹…sβˆ’22Gm_a/R = 100.1\ \text{m}^2\cdot\text{s}^{-2} has units of speed squared β€” take the square root.
❌ Check the units of RR. 316316 comes from R=4.0R = 4.0 instead of R=4.0Γ—103Β mR = 4.0 \times 10^{3}\ \text{m}; GG is in SI units, so the radius must be in metres.
Show solution

Set the total mechanical energy at launch to zero, since escape means arriving at infinity with Kf=0K_f = 0 and Uf=0U_f = 0:

12mvesc2βˆ’GmamR=0⟹vesc=2GmaR\tfrac{1}{2} m v_{\text{esc}}^2 - \frac{G m_a m}{R} = 0 \quad\Longrightarrow\quad v_{\text{esc}} = \sqrt{\frac{2 G m_a}{R}}

Substituting, with RR in metres:

2Gma=2(6.67Γ—10βˆ’11)(3.0Γ—1015)=4.00Γ—105Β m3β‹…sβˆ’22 G m_a = 2(6.67 \times 10^{-11})(3.0 \times 10^{15}) = 4.00 \times 10^{5}\ \text{m}^3\cdot\text{s}^{-2} 2GmaR=4.00Γ—1054.0Γ—103=100.1Β m2β‹…sβˆ’2\frac{2 G m_a}{R} = \frac{4.00 \times 10^{5}}{4.0 \times 10^{3}} = 100.1\ \text{m}^2\cdot\text{s}^{-2} vesc=100.1=10.0Β mβ‹…sβˆ’1v_{\text{esc}} = \sqrt{100.1} = 10.0\ \text{m}\cdot\text{s}^{-1}

Note that the escaping object's mass never entered β€” it cancelled in the first line.

Problem 2 Β· Pebble and Astronaut

Given: a 0.20Β kg0.20\ \text{kg} pebble and a 60Β kg60\ \text{kg} astronaut, both on Toro's surface, where vesc=7.3Β mβ‹…sβˆ’1v_{\text{esc}} = 7.3\ \text{m}\cdot\text{s}^{-1} β€” decide what each one needs in order to escape.

βœ… Correct! The mm in 12mv2=Gmtm/R\tfrac{1}{2}mv^2 = Gm_tm/R cancels, so the speed is common; but K=12mvesc2K = \tfrac{1}{2}mv_{\text{esc}}^2 still carries it: 5.3Β J5.3\ \text{J} for the pebble against 1.6Γ—103Β J1.6 \times 10^{3}\ \text{J} for the astronaut.
❌ The speed is right, the energy is not. K=12mvesc2K = \tfrac{1}{2}mv_{\text{esc}}^2 is proportional to mm: 12(0.20)(53.4)=5.3Β J\tfrac{1}{2}(0.20)(53.4) = 5.3\ \text{J} versus 12(60)(53.4)=1.6Γ—103Β J\tfrac{1}{2}(60)(53.4) = 1.6 \times 10^{3}\ \text{J}.
❌ The well really is deeper β€” but so is the tank. UU and KK both scale with mm, so mm divides out of 12mv2=Gmtm/R\tfrac{1}{2}mv^2 = Gm_tm/R and the required speed is unchanged.
❌ Inertia does not enter. vesc=2Gmt/Rv_{\text{esc}} = \sqrt{2Gm_t/R} contains only the asteroid's mass and radius; the escaping object's mass has already cancelled.
Show solution

Zero total mechanical energy at launch gives, for an object of any mass mm:

12mvesc2=GmtmR⟹vesc=2GmtR=7.3Β mβ‹…sβˆ’1\tfrac{1}{2} m v_{\text{esc}}^2 = \frac{G m_t m}{R} \quad\Longrightarrow\quad v_{\text{esc}} = \sqrt{\frac{2 G m_t}{R}} = 7.3\ \text{m}\cdot\text{s}^{-1}

Both terms are proportional to mm, so mm cancels and the speed is identical for both objects.

The energy needed is not. With vesc2=53.4Β m2β‹…sβˆ’2v_{\text{esc}}^2 = 53.4\ \text{m}^2\cdot\text{s}^{-2}:

Kpebble=12(0.20)(53.4)=5.3Β J,Kastronaut=12(60)(53.4)=1.6Γ—103Β JK_{\text{pebble}} = \tfrac{1}{2}(0.20)(53.4) = 5.3\ \text{J}, \qquad K_{\text{astronaut}} = \tfrac{1}{2}(60)(53.4) = 1.6 \times 10^{3}\ \text{J}

The ratio is exactly the mass ratio, 60/0.20=30060/0.20 = 300.

Problem 3 Β· Launched Too Slowly

Given: an object leaves Toro's surface radially at v0=5.0Β mβ‹…sβˆ’1v_0 = 5.0\ \text{m}\cdot\text{s}^{-1}, with Gmt=1.334Γ—105Β m3β‹…sβˆ’2G m_t = 1.334 \times 10^{5}\ \text{m}^3\cdot\text{s}^{-2} and R=5.0Γ—103Β mR = 5.0 \times 10^{3}\ \text{m} β€” find its total mechanical energy per kilogram and the greatest distance from Toro's centre that it reaches.

Total mechanical energy per kilogram at launch

Greatest distance from Toro's centre

βœ… Correct! E/m=12.5βˆ’26.68=βˆ’14.18Β Jβ‹…kgβˆ’1E/m = 12.5 - 26.68 = -14.18\ \text{J}\cdot\text{kg}^{-1} is negative, so the object is bound; at the turning point K=0K = 0 and βˆ’Gmt/r=βˆ’14.18-Gm_t/r = -14.18 gives r=9.41Γ—103Β mr = 9.41 \times 10^{3}\ \text{m}.
❌ That is K/mK/m alone. The gravitational potential energy at the surface, βˆ’Gmt/R=βˆ’26.68Β Jβ‹…kgβˆ’1-Gm_t/R = -26.68\ \text{J}\cdot\text{kg}^{-1}, still has to be added in.
❌ That is U/mU/m alone. Add the launch kinetic energy 12v02=12.5Β Jβ‹…kgβˆ’1\tfrac{1}{2}v_0^2 = 12.5\ \text{J}\cdot\text{kg}^{-1} to the well depth.
❌ Check the sign of KK. Kinetic energy is positive: E/m=+12.5βˆ’26.68E/m = +12.5 - 26.68, not βˆ’12.5βˆ’26.68-12.5 - 26.68.
❌ Not quite. E/m=12v02βˆ’Gmt/RE/m = \tfrac{1}{2}v_0^2 - Gm_t/R, with 12(5.0)2=12.5\tfrac{1}{2}(5.0)^2 = 12.5 and Gmt/R=26.68Β Jβ‹…kgβˆ’1Gm_t/R = 26.68\ \text{J}\cdot\text{kg}^{-1}.
❌ That is the altitude, not the distance from the centre. 4.4 km4.4\ \text{km} is the height above the surface; add Toro's radius R=5.0 kmR = 5.0\ \text{km}.
❌ That assumes constant gravity. Using h=v02/2gh = v_0^2/2g with g=5.34Γ—10βˆ’3Β mβ‹…sβˆ’2g = 5.34 \times 10^{-3}\ \text{m}\cdot\text{s}^{-2} gives 2.3Β km2.3\ \text{km}, but gg falls off badly over that distance β€” use U=βˆ’Gmtm/rU = -Gm_t m/r instead.
❌ The initial potential energy was dropped. r=2Gmt/v02=10.7 kmr = 2Gm_t/v_0^2 = 10.7\ \text{km} comes from setting 12v02=Gmt/r\tfrac{1}{2}v_0^2 = Gm_t/r, which forgets that the object started already deep in the well.
❌ Not quite. At the highest point K=0K = 0, so the total energy is entirely potential: βˆ’Gmt/rmax⁑=E/m-Gm_t/r_{\max} = E/m.
Show solution

Step 1 β€” Total mechanical energy per kilogram at launch.

Em=12v02βˆ’GmtR=12(5.0)2βˆ’1.334Γ—1055.0Γ—103=12.5βˆ’26.68=βˆ’14.18Β Jβ‹…kgβˆ’1\frac{E}{m} = \tfrac{1}{2}v_0^2 - \frac{G m_t}{R} = \tfrac{1}{2}(5.0)^2 - \frac{1.334 \times 10^{5}}{5.0 \times 10^{3}} = 12.5 - 26.68 = -14.18\ \text{J}\cdot\text{kg}^{-1}

It is negative, so 5.0Β mβ‹…sβˆ’15.0\ \text{m}\cdot\text{s}^{-1} is below the 7.3Β mβ‹…sβˆ’17.3\ \text{m}\cdot\text{s}^{-1} escape velocity and the object is bound.

Step 2 β€” The turning point. At the greatest distance the object is momentarily at rest, so K=0K = 0 and all of EE is potential. Energy is conserved, so that value is still βˆ’14.18Β Jβ‹…kgβˆ’1-14.18\ \text{J}\cdot\text{kg}^{-1}:

βˆ’Gmtrmax⁑=βˆ’14.18⟹rmax⁑=1.334Γ—10514.18=9.41Γ—103Β m-\frac{G m_t}{r_{\max}} = -14.18 \quad\Longrightarrow\quad r_{\max} = \frac{1.334 \times 10^{5}}{14.18} = 9.41 \times 10^{3}\ \text{m}

So rmax⁑=9.4Β kmr_{\max} = 9.4\ \text{km} from the centre β€” about 1.9R1.9R, or 4.4Β km4.4\ \text{km} above the surface β€” and then it falls back.

Problem 4 Β· The Same Rock, Twice the Size

Given: a second asteroid made of the same material as Toro (same uniform density) but with twice the radius, Rβ€²=10.0Β kmR' = 10.0\ \text{km}, while Toro has mt=2.0Γ—1015Β kgm_t = 2.0 \times 10^{15}\ \text{kg}, R=5.0Β kmR = 5.0\ \text{km} and vesc=7.3Β mβ‹…sβˆ’1v_{\text{esc}} = 7.3\ \text{m}\cdot\text{s}^{-1} β€” find the escape velocity from the larger body.

βœ… Correct! Equal density means m∝R3m \propto R^3, so mβ€²=8mt=1.6Γ—1016Β kgm' = 8m_t = 1.6 \times 10^{16}\ \text{kg} and vescβ€²=2Gmβ€²/Rβ€²=213.4=14.6Β mβ‹…sβˆ’1v'_{\text{esc}} = \sqrt{2Gm'/R'} = \sqrt{213.4} = 14.6\ \text{m}\cdot\text{s}^{-1} β€” twice Toro's, and now beyond a 12Β mβ‹…sβˆ’112\ \text{m}\cdot\text{s}^{-1} sprint.
❌ Escape velocity does not fall with size here. vesc=2Gm/Rv_{\text{esc}} = \sqrt{2Gm/R} drops with RR only at fixed mass; at fixed density the mass grows as R3R^3, which wins.
❌ The mass was held fixed. 2Gmt/Rβ€²=5.2\sqrt{2Gm_t/R'} = 5.2 doubles the radius but keeps Toro's mass; the same rock at twice the radius is 88 times as massive.
❌ Escape velocity is not a property of the material alone. With m∝R3m \propto R^3, vesc=2Gm/R∝Rv_{\text{esc}} = \sqrt{2Gm/R} \propto R β€” it doubles when the radius doubles.
Show solution

Step 1 β€” Same density, so the mass scales as the volume.

mβ€²=mt(Rβ€²R)3=(2.0Γ—1015)(2)3=1.6Γ—1016Β kgm' = m_t \left(\frac{R'}{R}\right)^3 = (2.0 \times 10^{15})(2)^3 = 1.6 \times 10^{16}\ \text{kg}

Step 2 β€” Escape velocity of the bigger body.

vescβ€²=2Gmβ€²Rβ€²=2(6.67Γ—10βˆ’11)(1.6Γ—1016)1.0Γ—104=213.4=14.6Β mβ‹…sβˆ’1v'_{\text{esc}} = \sqrt{\frac{2 G m'}{R'}} = \sqrt{\frac{2(6.67 \times 10^{-11})(1.6 \times 10^{16})}{1.0 \times 10^{4}}} = \sqrt{213.4} = 14.6\ \text{m}\cdot\text{s}^{-1}

The scaling directly. With ρ\rho fixed, m=43πρR3m = \tfrac{4}{3}\pi\rho R^3, so

vesc=2GRβ‹…43πρR3=R83Ο€GΟβ€…β€Šβˆβ€…β€ŠRv_{\text{esc}} = \sqrt{\frac{2G}{R} \cdot \tfrac{4}{3}\pi\rho R^3} = R\sqrt{\tfrac{8}{3}\pi G \rho} \;\propto\; R

Doubling the radius doubles the escape velocity: 2Γ—7.3=14.6Β mβ‹…sβˆ’12 \times 7.3 = 14.6\ \text{m}\cdot\text{s}^{-1}. Since 14.6>1214.6 > 12, an Olympic sprinter could no longer outrun this asteroid's gravity.

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