To calculate the drag force, it is assumed that the drag coefficient (CD) is typically around 2.2 and that the cross-sectional area (A) of Starlink satellites is approximately 15.45 m2 (Hardy 2020). We attempted to examine the decay of altitude on Starlink satellites using the Two Line ...
you will need to enter the type of bullet and grain weight as well as the bullet’s Ballistic Coefficient (BC) figures. Weather conditions, as in altitude, temperature, and barometric pressures will be addressed. You’ll need the exact range or ranges you’re going to be shooting, and the...