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TheThe ffirirstt,, second, and thirthihirrd cosmmicic veloelocitiitieses anndd bllaack holholeses

The first cosmic is known as the orbital velocity, which is the least velocity of a projectile to keep the around a celestial body. When the centripetal and gravitational are in equilibrium, the object can hold the orbit. Let’s consider the ’s surface. mv 2 mM 1 = G E r r 2 Then, this velocity is obtained as GM v = E = 7.91×103 m/s 1 r −11 where G is the , 6.67 ×10 m3 kg-1 S-2. ME is the of the Earth, 5.972×1024 kg; and r is the Earth’s radius, 6371×103 m.

The second cosmic velocity is known as the . This is the velocity that escapes from the of a celestial body. This will be obtained by the conservation. 1 GM m mv 2 − E = 0 2 2 r Thus, we can calculate it for Earth’s surface. 2GM v = E = 11.2×103 m/s 2 r

The third cosmic velocity is the velocity that can escape from the gravitational field of the . Consider the orbit of the Earth around the and = × 11 this radius is rE 1.50 10 m. The velocity is calculated from the energy conservation with the of the Sun.

= × 30 The mass of the Sun is M S 1.99 10 kg. The velocity will become 2GM = S = × 3 vS 42 1. 10 m/s rE

This is the velocity from the reference frame of the Sun; therefore, we have to subtract the orbital velocity from the above velocity. Earth’s orbital velocity can be obtained from the centripetal and gravitational force from the Sun.

GM = S = × 3 vorbit 29 8. 10 m/s rE

Thus, the escape velocity from the orbit is

= − = × 3 vo−S vS vorbit 12 3. 10 m/s

Now, consider the velocity from the surface of the Earth, which becomes the third cosmic velocity.

1 2 GM E m 1 2 mv − = mv − 2 3 r 2 o S

2GM E 2 3 v = + v − = 16 7. ×10 m/s 3 r o S