Solar Powered Spaceship

The sun puts out roughly 4 × 1 0 26 4 \times 10^{26} Watts of electromagnetic energy. The sun emits as a blackbody at roughly 6000 K. The peak wavelength of the solar emission, i.e. the wavelength at which the intensity is highest, is approximately 500 nm (which is green). For the purposes of this discussion, let's assume all of the sun's radiation comes out at this wavelength. If we think about the radiation as photons, each photon carries a momentum given by p = h / λ p=h/\lambda and an energy E = h c / λ E=hc/\lambda by quantum mechanics.

One can use the electromagnetic radiation to propel spaceships, although it doesn't work all that well even though it is cheap. Consider a spaceship propelled by a "solar sail", a perfectly square reflecting sheet of material 1 km on a side oriented so the normal points directly towards the sun. At the earth's orbit, how much force in Newtons would such a solar sail experience?

Details and Assumptions

  • The earth orbits at a distance of roughly 1.5 × 1 0 8 1.5 \times 10^8 km from the sun.
  • The speed of light is 3 × 1 0 8 3 \times 10^8 m/s.
  • Planck's constant is h = 6.63 × 1 0 34 kg m 2 /s h=6.63\times 10^{-34}\text{ kg}\cdot\text{m}^2\text{/s} .


The answer is 9.43.

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3 solutions

Anish Puthuraya
Jan 24, 2014

Firstly,
Let us calculate the power that is received by the sheet at that distance.

P r e c e i v e d = P s u n 4 π d 2 P_{received} = \frac{P_{sun}}{4\pi d^2}\cdot Area of the sheet

Thus,
P r e c e i v e d = 4 × 1 0 26 4 π ( 1.5 × 1 0 11 ) 2 ( 1 0 3 ) 2 = 1 , 414 , 710 , 605 P_{received} = \frac{4\times10^{26}}{4\pi(1.5\times10^{11})^2} (10^3)^2 = 1,414,710,605 Watts

Now,
Since the Power is received in the form of photons ,
P r e c e i v e d = η × P_{received} = \eta\times Energy of each Photon ,
where η \eta represents the number of photons received by the sheet per unit time

Therefore,
η h c λ = 1 , 414 , 710 , 605 \eta \cdot \frac{hc}{\lambda} = 1,414,710,605

Also, note that the Change in Momentum of each photon as it reflects off the sheet is 2 p 2p

Hence,
Force = d p t o t a l d t = η × 2 p = η × 2 h λ = \frac{dp_{total}}{dt} = \eta \times 2p = \eta \times \frac{2h}{\lambda}

\Rightarrow Force = 1 , 414 , 710 , 605 × λ h c × 2 h λ = 1,414,710,605 \times \frac{\lambda}{hc} \times \frac{2h}{\lambda}

\Rightarrow Force = 1 , 414 , 710 , 605 × 2 3 × 1 0 8 9.43 N = \frac{1,414,710,605\times2}{3\times10^8} \approx \boxed{9.43N}

excellent solution ..

soyu matthew - 7 years, 4 months ago

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Thanks.

Anish Puthuraya - 7 years, 4 months ago
Steven Zheng
Jul 24, 2014

Notice that the particle absorbs the radiation, then reflecting it back. Thus the change in momentum is Δ p = 2 Δ U c . \Delta p = \frac{2 \Delta U}{c}. Since the change in energy is equal P Δ t P\Delta t , where P P is the power of the sun, we get Δ U = A I Δ t , \Delta U = AI\Delta t, where A and I denote area of the sail and the intensity of the sun. We know F Δ t = Δ p F\Delta t = \Delta p , consequently, F = 2 A I c . F = \frac{2AI}{c}.

Chew-Seong Cheong
Aug 21, 2014

The solar power per unit area when it reach Earth and the solar sail:

Δ P s = P s 4 π R 2 = 4 × 1 0 26 4 π ( 1.5 × 1 0 11 ) 2 = 1414.710605 W / m 2 \Delta P_s = \cfrac{P_s}{4\pi R^2} = \cfrac{4\times 10^{26}}{4\pi (1.5\times 10^{11})^2}=1414.710605W/m^2

The radiation power collected by the 1-km square solar sail:

P s a i l = Δ P s A = 1414.710605 × 1 0 6 = 1414710605 W P_{sail} = \Delta P_sA = 1414.710605 \times 10^6 = 1414710605W

Since all the radiation power is converted to mechanical power and that E = h c λ = c p E=\cfrac{hc}{\lambda}=cp \Rightarrow momentum p = E c p=\cfrac{E}{c} , then the force:

F = d p d t = 2 × P s a i l c = 2 × 1414710605 300000000 = 9.43 N F = \cfrac{dp}{dt} = 2\times \cfrac{P_{sail}}{c}= 2\times \cfrac{1414710605}{300000000}= \boxed{9.43N}

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