Spacecraft have been sent to Mars in recent years. Mars is smaller than Earth and has correspondingly weaker surface gravity. On Mars, the free-fall acceleration is only 3.8m/s2 .What is the orbital period of a spacecraft in a low orbit near the surface of Mars? Assume the radius of the satellite's orbit is about the same as the radius of Mars itself, rMars = 3.37

Respuesta :

The orbital period of the spacecraft is about 5.9 × 10³ s ≈ 99 minutes

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Further explanation

Let's recall Centripetal Force formula as follows:

[tex]\boxed{F = m \frac{v^2}{R}}[/tex]

where:

F = Centripetal Force ( Newton )

m = mass of object ( kg )

v = speed of object ( m/s )

R = radius ( m )

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Newton's gravitational law states that the force of attraction between two objects can be formulated as follows:

[tex]\boxed {F = G \frac{m_1 ~ m_2}{R^2}}[/tex]

where:

F = Gravitational Force ( Newton )

G = Gravitational Constant ( 6.67 × 10⁻¹¹ Nm² / kg² )

m = Object's Mass ( kg )

R = Distance Between Objects ( m )

Let us now tackle the problem !

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Given:

free-fall acceleration = g = 3.8 m/s²

radius of Mars = R = 3.37 × 10⁶ m

Asked:

orbital period = T = ?

Solution:

[tex]\Sigma F = ma[/tex]

[tex]G \frac{ M m} { R^2 } = m \omega^2 R[/tex]

[tex]G \frac{ M } { R^2 } = \omega^2 R[/tex]

[tex]g = \omega^2 R[/tex]

[tex]\omega^2 = g \div R[/tex]

[tex]\omega = \sqrt { g \div R }[/tex]

[tex]2 \pi \div T = \sqrt { g \div R }[/tex]

[tex]T = 2 \pi \div \sqrt { g \div R [/tex]

[tex]T = 2 \pi \sqrt{ R \div g}[/tex]

[tex]T = 2 \pi \sqrt{ 3.37 \times 10^6 \div 3.8 }[/tex]

[tex]\boxed{T \approx 5.9 \times 10^3 \texttt{ s}}[/tex]

[tex]\boxed{T \approx 99 \texttt{ minutes}}[/tex]

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Answer details

Grade: High School

Subject: Physics

Chapter: Gravitational Fields

Ver imagen johanrusli

The orbital period of a spacecraft in a low orbit near the surface of Mars is

  • 5.9 * 10³ secs

Given data:

The free-fall acceleration ( g ) = 3.8 m/s²

Radius of the satellite orbit = Radius of Mars ( rMars ) = 3.37 * 10⁶

Orbital period ( T ) = ?

R ( radius ) = 3.37 * 10⁶

Determine the orbital period of a spacecraft using the formula below

∑F = ma

where ; F = G [tex]\frac{M}{R^{2} } = w^{2} R[/tex]

g = [tex]w^{2} R[/tex]

where ; [tex]w = 2\pi / T[/tex]

∴ T = [tex]2\pi / \sqrt{R/g}[/tex]

     = [tex]2\pi / \sqrt{3.37*10^{6} / 3.8 }[/tex]

T = 5.9 * 10³ secs

Hence the orbital period of a spacecraft in a low orbit near the surface of mars is 5.9 * 10³ secs .

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