System and method for launching multiple satellites from a launch vehicle

A method for deploying and launching multiple satellites using a mechanical structure at a launching vehicle, said method comprising:

• positioning said multiple satellites in a plurality of mounts provided in said mechanical structure, wherein said mounts are arranged at a distance to satisfy a collision free requirement based on a maximum collision probability (Pmax);
• a separating step of separating a first set of satellites in an axial direction and a second set of satellites in a radial direction;
• dividing a second set of satellites into two groups based on a velocity direction and an anti-velocity direction;
• a re-orienting step of re-orienting a stage and separating the satellites grouped under any one of said two groups with a roll rate between 0.20 to 0.35 degrees to ensure separation of satellites in an orbital plane along the velocity and anti-velocity directions;
• and
• launching said first set of satellites arranged in the axial direction, a part of said second set of satellites arranged in the radial direction and a remaining part of said second set of satellites arranged in an inclined direction from said launch vehicle to separate said first and second sets of satellites with in-track delta v distribution.