Gravitational Field Flashcards
Gravitational force between point masses( vector ) Gravitation field ( vector) Gravitational potential ( scalar) Circular orbits
Newton’s law of Gravitation
the mutual force of attraction between any two point masses is directly proportional to the product of their masses and inversely proportional to the square of the separation between their centres
F = G m₁ m₂ / r²
F magnitude of gravitational force [N]
G gravitational constant 6.67 × 10-¹¹ N m² kg⁻¹
m₁ one of the point masses [kg]
m₂ other point mass [kg]
r centre to centre distance between the two point masses [m]
Gravitational field
Region of space surrounding a body in which another body placed in it experiences a gravitational force due to its mass
Gravitational field strength g at a particular point in the gravitational field
gravitational force exerted per unit mass on a small test mass placed at that point
g = GM/ r²
g magnitude of gravitational field strength at point [N kg⁻¹]
G gravitational constant 6.67 × 10⁻¹¹ N m² kg⁻²
M source mass that generates the gravitational field [kg]
r distance from centre of source mass M to point X [m]
Gravitational potential energy U of a point mass placed at a point in the gravitational field
work done in bringing the point mass from infinity to that point
Gravitational potential energy U of the M-m system [J]
U = - GMm/r
G gravitational constant 6.67 × 10⁻¹¹ N m² kg⁻²
M one of the point mass [kg]
m other point mass [kg]
r centre-to-cetre distance between the two point masses [m]
The escape speed/ velocity for an object at the Earth’s surface
minimum speed it must have at the start to escape from the gravitational influence of the Earth
v = √( 2GMe/Re)
Gravitational potential φ at a point in the gravitational field
work done per unit mass in bringing a small test mass from infinity to that point
φ = -GM/r
φ gravitational potential at point X [ J kg⁻¹]
G gravitational constant 6.67 × 10⁻¹¹ N m² kg⁻²
M source mass that generates the gravitational field [kg]
r distance from centre of point mass M to point X [m]
relation of F to U
F - δU/ δr
relation of g to φ
g = - δφ/δr
orbiting speed of satellite
Fg provides Fc
v = √ ( GM /r)
energy of satellite in orbit
Ek = 1/2 m v²
= GMm/2r
Ep = - GMm/r
Et = - GMm/2r
Et = - Ek
= 1/2 Ep
Kepler’s third law
Fg provides Fc
GMm/r² = mrω² , ω = 2π/T
T² = 4π²r³/GM
T² ∝ r³
Geostationary satellite
rotates around planet such that it is always positioned above same point on the planet’s surface
Conditions for satellite moving in geostationary orbit for Earth
- placed above equator - same axis of rotation
- move from west to east - same direction as rotation of Earth about its own axis
- satellite orbital period = 24h - same as Earth’s rotational period about it’s own axis
Advantages and disadvantages of geostationary satellite
Advantages
- same relative position to Earth’s surface, allows continuous and uninterrupted signal transmission- telecommunications
- positioned at high altitudes, scan a large section of Earth’s surface - weather imaging
Disadvantages
- high altitudes ; poor resolution, delay in reception hence lag, expensive to launch
- weak signal received by transmitting stations of countries with latitudes above 60° due larger amount of atmosphere