☰ Contents · Astronomy

Calculating masses and cosmic velocities

Lessons 26–27 · 2 lessons · M. Mamadazimov. Astronomy Grade 11, 1st edition. DAVR NASHRIYOTI, Tashkent, 2018
27

The two-body problem. Cosmic velocities

Textbook: pp. 45–46
GoalExplain the two-body problem, the types of orbit and the cosmic velocities (first, second, third) and calculate with them.
New words
two-body problem · ikki jism masalasifirst cosmic velocity · birinchi kosmik tezlikescape velocity · ikkinchi kosmik tezlikconic section · kon kesimi
Explanation

The two-body problem: two bodies moving only under their mutual gravity move about their common centre of mass along a conic section – circle, ellipse, parabola or hyperbola; the shape depends on the total energy: negative gives an ellipse (bound orbit), zero a parabola, positive a hyperbola. The first cosmic velocity v₁ = √(GM/R) is needed to circle near the surface: ≈ 7.9 km/s for the Earth. The second (escape) velocity v₂ = √2 · v₁ ≈ 11.2 km/s is enough to leave the Earth for infinity. The third cosmic velocity v₃ ≈ 16.7 km/s is needed to leave the Solar System from near the Earth (launching in the direction of the Earth’s orbital motion to use its speed). Escape speeds at other bodies: the Moon ≈ 2.4 km/s, Mars ≈ 5.0 km/s, Jupiter ≈ 59.5 km/s.

Worked examples
Circling a 40,000 km orbit near the Earth at ≈ 8 km/s takes t = 40,000 : 8 = 5000 s ≈ 84 minutes.
The first cosmic velocity of Mars is ≈ 3.6 km/s: v₂ = √2 · 3.6 ≈ 5.0 km/s – matching the table.
Class activity

Paper-and-ball model: roll a ball off a table edge at increasing horizontal speeds and watch it land farther (Newton’s cannonball idea); imagine that at high enough speed it would go round the Earth. Use only a soft ball.

Practice
1
When is an orbit an ellipse, a parabola or a hyperbola?
2
At 8 km/s near the Earth, in how many seconds does a body cover 32,000 km?
3
Why is the second cosmic velocity √2 times the first?
4
Why does the Moon have almost no atmosphere?