The moon is a vacuum for all practical purposes, especially at 50km altitude.mfb said:In 50km, there is nothing which I would call orbit, there is too much air drag.
The impact velocity vector for orbital trajectory is the velocity at which an object approaches a target during its orbital motion. It includes both the magnitude and direction of the velocity, and is an important factor in determining the outcome of an orbital mission.
The impact velocity vector for orbital trajectory can be computed using mathematical equations and calculations based on the initial velocity, gravitational forces, and other factors such as atmospheric drag. This can be done using specialized software or by hand using formulas and data from the orbital mission.
Computing the impact velocity vector for orbital trajectory is crucial for ensuring a successful orbital mission. It allows scientists to accurately predict the path and velocity of an object, and make necessary adjustments to ensure it reaches its target without any complications or collisions.
Several factors can affect the impact velocity vector for orbital trajectory, including the mass and speed of the object, gravitational forces, atmospheric conditions, and any external forces acting on the object. These must all be taken into account when computing the impact velocity vector.
Yes, the impact velocity vector for orbital trajectory can be altered during the mission through various methods such as thrusting, aerobraking, and gravity assists. These maneuvers can change the magnitude and direction of the velocity to achieve the desired impact on the target.