9702/42

Physics 9702/42May/June 2016

Cambridge A-Level · A Level Structured Questions · worked solutions for every part, with the mark scheme

13
questions
100
marks
120
minutes

Topics Gravitational Fields · Magnetic Fields · Motion in a Circle · Ideal Gases · Temperature · Oscillations · +8 more

Q1Gravitational FieldsMotion in a CircleFree sample

A binary star consists of two stars A and B that orbit one another, as illustrated in Fig. 1.1.

The stars are in circular orbits with the centres of both orbits at point P, a distance dd from the centre of star A.

(a)
(i)

Explain why the centripetal force acting on both stars has the same magnitude.

2M
DifficultyMedium-Easy
Worked solution

Answer

The centripetal force on each star is provided by the gravitational attraction between the two stars.

By Newton’s third law, the gravitational force exerted by A on B has the same magnitude as the force exerted by B on A (equal and opposite pair), so the centripetal forces on the two stars have the same magnitude.

Final answer

The centripetal force is the mutual gravitational force, which has equal magnitude on each star by Newton’s third law.

Detailed explanation

Background Concept

In a binary system, each star is kept in circular motion by a centripetal force directed towards the centre of its circular path.

If the only significant interaction is gravity, the centripetal force is just the gravitational force of attraction between the two masses:

F=Gm1m2r2F = \frac{G m_1 m_2}{r^2}

Newton’s third law says that forces in an interaction pair are equal in magnitude and opposite in direction: “force on A due to B” equals “force on B due to A” in magnitude.

Understanding the Question

We are told both stars move in circles about the same point P. The question asks why the centripetal forces on A and B are equal in magnitude.

Even though their masses and orbit radii may be different, the force responsible for both circular motions comes from the same two-body interaction.

Approach

  1. Identify what provides the centripetal force (gravity between the stars).
  2. Use Newton’s third law to compare the force on A with the force on B.

Step-by-Step Reasoning

  • Star A attracts star B gravitationally; star B attracts star A gravitationally.
  • These two forces form a Newton’s third law pair, so their magnitudes are equal.
  • Each force acts towards the other star (along the line joining their centres), which is also the direction towards the centre of the circular motion about P at that instant.
  • Therefore, the centripetal force on A and the centripetal force on B have the same magnitude (but act on different bodies, in opposite directions).

Key Takeaways

  • In two-body gravity problems, the forces on the two bodies are always equal in magnitude (Newton’s third law).
  • The centripetal force is not a new force; it is the name for the resultant inward force causing circular motion.

Common Mistakes

  • Saying the centripetal forces are equal because the stars have the same angular speed (that alone does not force equal centripetal force because F=mrω2F = m r \omega^2 depends on mm and rr).
  • Mixing up “same magnitude” with “same direction” (directions are opposite).

Things to Be Careful About

  • Be explicit that the centripetal force is the gravitational attraction.
  • State Newton’s third law clearly: equal magnitude, opposite direction, acting on different bodies.
Techniques used
identify the centripetal force as the mutual gravitational attractionapply Newton's third law to an interacting pairlink equal-and-opposite interaction forces to equal force magnitudes on each body
(ii)

The period of the orbit of the stars about point P is 4.0 years.

Calculate the angular speed ω\omega of the stars.

ω\omega = ______ rad s1\text{rad s}^{-1}

2M
DifficultyMedium-Easy
Worked solution

Working

T=4.0 years=4.0×365×24×3600=1.26×108 sT = 4.0\ \text{years} = 4.0 \times 365 \times 24 \times 3600 = 1.26 \times 10^8\ \text{s} ω=2πT=2π1.26×108=4.98×108 rad s1\omega = \frac{2\pi}{T} = \frac{2\pi}{1.26 \times 10^8} = 4.98 \times 10^{-8}\ \text{rad s}^{-1}

Answer

ω5.0×108 rad s1\omega \approx 5.0 \times 10^{-8}\ \text{rad s}^{-1}
Final answer

5.0 × 10^-8 rad s^-1

Detailed explanation

Background Concept

For uniform circular motion, the angular speed ω\omega is the rate of change of angular displacement (in radians) per second. One complete orbit corresponds to an angular displacement of 2π2\pi radians, so

ω=2πT\omega = \frac{2\pi}{T}

where TT is the period (time for one full orbit).

Understanding the Question

The stars complete one orbit about point P in 4.04.0 years. We need the angular speed in rad s1\text{rad s}^{-1}, so the period must be converted into seconds before using ω=2π/T\omega = 2\pi/T.

Approach

  1. Convert T=4.0T = 4.0 years into seconds.
  2. Substitute into ω=2π/T\omega = 2\pi/T.
  3. Round appropriately (typically 2 s.f. because 4.04.0 has 2 s.f.).

Step-by-Step Reasoning

  • Convert years to seconds:
T=4.0×365 days×24 h day1×3600 s h1T = 4.0 \times 365\ \text{days} \times 24\ \text{h day}^{-1} \times 3600\ \text{s h}^{-1} T=1.26×108 sT = 1.26 \times 10^8\ \text{s}
  • Now calculate angular speed:
ω=2π1.26×108=4.98×108 rad s1\omega = \frac{2\pi}{1.26 \times 10^8} = 4.98 \times 10^{-8}\ \text{rad s}^{-1}
  • Rounding to 2 significant figures gives:
ω5.0×108 rad s1\omega \approx 5.0 \times 10^{-8}\ \text{rad s}^{-1}

Key Takeaways

  • Always convert the period into SI units (seconds) when angular speed is required in rad s1\text{rad s}^{-1}.
  • One full revolution is 2π2\pi radians.

Common Mistakes

  • Leaving the period in years and giving ω\omega in rad year1\text{rad year}^{-1}.
  • Using ω=π/T\omega = \pi/T instead of 2π/T2\pi/T.
  • Rounding too early (carry at least 3 s.f. in intermediate steps).

Things to Be Careful About

  • Use standard form correctly when dividing by a large number.
  • The unit is rad s1\text{rad s}^{-1} (radian is dimensionless but the unit is still written).
Techniques used
use \(\omega = 2\pi/T\) for uniform circular motionconvert a time period into secondssubstitute into an equation and round to appropriate significant figures
(b)

The separation of the centres of the stars is 2.8×108 km2.8 \times 10^8\ \text{km}.
The mass of star A is MAM_A. The mass of star B is MBM_B.
The ratio MAMB\frac{M_A}{M_B} is 3.0.

(i)

Determine the distance dd.

dd = ______ km\text{km}

3M
DifficultyMedium
Worked solution

Working

For orbit about the centre of mass at P:

MAd=MB(2.8×108d)M_A d = M_B (2.8 \times 10^8 - d)

Given MA/MB=3.0M_A/M_B = 3.0:

3d=2.8×108d    4d=2.8×1083d = 2.8 \times 10^8 - d \;\Rightarrow\; 4d = 2.8 \times 10^8 d=7.0×107 kmd = 7.0 \times 10^7\ \text{km}

Answer

d=7.0×107 kmd = 7.0 \times 10^7\ \text{km}
Final answer

7.0 × 10^7 km

Detailed explanation

Background Concept

If two objects orbit each other under mutual forces, they actually orbit about their common centre of mass. For two masses on a line,

MArA=MBrBM_A r_A = M_B r_B

where rAr_A and rBr_B are their distances from the centre of mass (here point P), measured along the line joining them.

Also, the total separation of their centres is

rA+rB=Rr_A + r_B = R

where RR is the distance between the stars.

Understanding the Question

The distance between the star centres is R=2.8×108 kmR = 2.8 \times 10^8\ \text{km}. Point P is the common centre of the circular orbits (centre of mass). The distance from A to P is dd, so rA=dr_A = d and rB=Rdr_B = R - d.

We are given MA/MB=3.0M_A/M_B = 3.0 and asked to find dd.

Approach

  1. Use the centre-of-mass condition MAd=MB(Rd)M_A d = M_B (R-d).
  2. Substitute the mass ratio to get a single equation in dd.
  3. Solve for dd.

Step-by-Step Reasoning

  • Write the centre-of-mass relation about P:
MAd=MB(Rd)M_A d = M_B (R - d)
  • Use MA=3.0MBM_A = 3.0 M_B:
(3.0MB)d=MB(Rd)(3.0 M_B)d = M_B(R-d)

Cancel MBM_B:

3d=Rd3d = R - d
  • Solve:
4d=R=2.8×108 km4d = R = 2.8 \times 10^8\ \text{km} d=2.8×1084=7.0×107 kmd = \frac{2.8 \times 10^8}{4} = 7.0 \times 10^7\ \text{km}

This makes sense: the more massive star A (three times heavier) is closer to P, so dd is smaller than R/2R/2.

Key Takeaways

  • Two-body circular motion happens about the centre of mass.
  • The condition MArA=MBrBM_A r_A = M_B r_B is extremely useful with given mass ratios.

Common Mistakes

  • Using MA/MB=d/(Rd)M_A/M_B = d/(R-d) instead of the correct inverted ratio (it should be MA/MB=(Rd)/dM_A/M_B = (R-d)/d).
  • Assuming P is midway between the stars (only true if masses are equal).

Things to Be Careful About

  • Keep distances consistent: rB=Rdr_B = R - d (not R+dR + d).
  • Units: here the question wants dd in km, so no conversion is needed in this part.
Techniques used
use the centre-of-mass condition for two orbiting bodiesset up simultaneous equations using total separationsolve a ratio relationship algebraically
(ii)

Use your answers in (a)(ii) and (b)(i) to determine the mass MBM_B of star B.
Explain your working.

MBM_B = ______ kg\text{kg}

3M
DifficultyMedium-Hard
Worked solution

Working

From (b)(i):

R=2.8×108 km=2.8×1011 mR = 2.8 \times 10^8\ \text{km} = 2.8 \times 10^{11}\ \text{m} rB=Rd=2.8×1087.0×107=2.1×108 km=2.1×1011 mr_B = R - d = 2.8 \times 10^8 - 7.0 \times 10^7 = 2.1 \times 10^8\ \text{km} = 2.1 \times 10^{11}\ \text{m}

For star B, gravitational force provides centripetal force:

GMAMBR2=MBrBω2\frac{G M_A M_B}{R^2} = M_B r_B \omega^2

Cancel MBM_B and use MA=3.0MBM_A = 3.0 M_B:

G(3.0MB)R2=rBω2\frac{G (3.0 M_B)}{R^2} = r_B \omega^2 MB=rBω2R23GM_B = \frac{r_B \omega^2 R^2}{3G}

Using ω=4.98×108 rad s1\omega = 4.98 \times 10^{-8}\ \text{rad s}^{-1} from (a)(ii):

MB=(2.1×1011)(4.98×108)2(2.8×1011)23(6.67×1011)M_B = \frac{(2.1 \times 10^{11})(4.98 \times 10^{-8})^2 (2.8 \times 10^{11})^2}{3(6.67 \times 10^{-11})} MB=2.0×1029 kgM_B = 2.0 \times 10^{29}\ \text{kg}

Answer

MB2.0×1029 kgM_B \approx 2.0 \times 10^{29}\ \text{kg}
Final answer

2.0 × 10^29 kg

Detailed explanation

Background Concept

For circular orbits, the required centripetal force is

Fc=mrω2F_c = m r \omega^2

where mm is the mass of the orbiting object, rr is its orbital radius about the centre of its circular path, and ω\omega is the angular speed.

In a binary star system, the inward force causing the circular motion is the gravitational attraction between the stars:

Fg=GMAMBR2F_g = \frac{G M_A M_B}{R^2}

where RR is the separation of their centres.

So we set Fg=FcF_g = F_c for either star, using the correct radius about point P.

Understanding the Question

We know:

  • Period T=4.0T = 4.0 years, so from (a)(ii) we have ω\omega.
  • Total separation of stars: R=2.8×108 kmR = 2.8 \times 10^8\ \text{km}.
  • From (b)(i), distance from A to P: d=7.0×107 kmd = 7.0 \times 10^7\ \text{km}.
  • Mass ratio: MA/MB=3.0M_A/M_B = 3.0.

We must find MBM_B in kg. This needs SI units: km to m, and use G=6.67×1011 N m2 kg2G = 6.67 \times 10^{-11}\ \text{N m}^2\ \text{kg}^{-2}.

Approach

  1. Find star B’s orbital radius about P: rB=Rdr_B = R - d.
  2. Write gravitational force between the stars and equate it to the centripetal force for star B.
  3. Cancel MBM_B where possible and use MA=3MBM_A = 3M_B to solve for MBM_B.

Step-by-Step Reasoning

  • Convert separation to metres:
R=2.8×108 km=2.8×1011 mR = 2.8 \times 10^8\ \text{km} = 2.8 \times 10^{11}\ \text{m}
  • Find star B’s orbital radius (distance from B to point P):
rB=(2.8×1087.0×107) km=2.1×108 km=2.1×1011 mr_B = (2.8 \times 10^8 - 7.0 \times 10^7)\ \text{km} = 2.1 \times 10^8\ \text{km} = 2.1 \times 10^{11}\ \text{m}
  • Equate forces for star B:
GMAMBR2=MBrBω2\frac{G M_A M_B}{R^2} = M_B r_B \omega^2
  • Cancel MBM_B (this is common in orbit problems):
GMAR2=rBω2\frac{G M_A}{R^2} = r_B \omega^2
  • Substitute MA=3MBM_A = 3M_B:
G(3MB)R2=rBω2\frac{G (3M_B)}{R^2} = r_B \omega^2
  • Rearrange for MBM_B:
MB=rBω2R23GM_B = \frac{r_B \omega^2 R^2}{3G}
  • Substitute numbers (using ω=4.98×108 rad s1\omega = 4.98 \times 10^{-8}\ \text{rad s}^{-1}):
MB2.0×1029 kgM_B \approx 2.0 \times 10^{29}\ \text{kg}

The result is of the order of a solar mass (2×1030 kg\approx 2 \times 10^{30}\ \text{kg}), which is reasonable for a star.

Key Takeaways

  • For circular gravitational orbits, set gravitational attraction equal to centripetal requirement.
  • Use the separation RR in the gravitational force, but the orbital radius about the centre of mass (rAr_A or rBr_B) in the centripetal term.
  • Mass ratios allow you to eliminate one mass.

Common Mistakes

  • Using rB=dr_B = d instead of rB=Rdr_B = R - d.
  • Mixing up the two different distances: RR (between stars) vs. rBr_B (from star B to P).
  • Forgetting to convert km to m, causing the mass to be wrong by a factor of 10310^3 or 10610^6.
  • Not cancelling MBM_B correctly, leading to unnecessary algebra.

Things to Be Careful About

  • Keep SI units throughout when using GG.
  • Use the angular speed from (a)(ii) in rad s1\text{rad s}^{-1}.
  • Square brackets and powers: R2R^2 is very large; handle standard form carefully to avoid exponent errors.
Techniques used
equate gravitational force to required centripetal forceuse the centre-of-mass distances to determine the orbital radiussubstitute a mass ratio to eliminate one unknownconvert km to m and years to seconds for SI consistency

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