What are the key factors affecting satellite orbits?
The key factors affecting satellite orbits are gravitational forces, atmospheric drag, solar radiation pressure, and the gravitational influence of the Moon and other celestial bodies. These factors can cause perturbations leading to changes in a satellite's speed, altitude, and orientation over time.
How do gravitational forces influence orbital stability?
Gravitational forces provide the centripetal force that maintains an object in a stable orbit. They ensure that the object continuously accelerates towards the central body, preventing it from drifting into space or crashing. Variations in gravitational forces, due to factors like elliptical orbits or external influences, can affect stability. Effective orbital parameters must be calculated to ensure long-term stability.
What are the common types of orbital manoeuvres?
The common types of orbital manoeuvres are Hohmann transfer, bi-elliptic transfer, and plane change manoeuvres. Other types include low-thrust spiral manoeuvres and gravity assists. These manoeuvres are used for changing a spacecraft's orbit, altitude, or inclination.
What are Lagrange points and why are they important in orbital dynamics?
Lagrange points are specific locations in space where the gravitational forces of two large bodies balance with the centripetal force felt by a smaller object. These points allow for stable positioning of satellites and space telescopes, making them essential for missions requiring consistent observational platforms.
How does atmospheric drag impact low Earth orbits?
Atmospheric drag causes gradual orbital decay for satellites in low Earth orbits by reducing their altitude and velocity over time. This drag depends on the atmospheric density, which increases as altitude decreases, leading to more significant deceleration and eventually re-entry if no corrective measures are taken.