dinos55

Thank you all!

Hello all, If a rocket has 3 stages + upper stage, and the details I know are the total mass of the rocket, the inclination and the Propellant Mass, the Thrust, The Isp(specific impulse) and the combustion time, for each stage. Can I find the mass of the payload and the altitude of the orbit using these details? and if yes, how? Thanking you in advance.

@OhioBob thank you again for your help!

@regex thank you very much!

thank you both for your answers! @OhioBob @regex I would like to ask you something more. How can I find the revolutions that the satellite will do with electric propulsion until it reaches geo from leo? and the total time is t=deltav/acceleration(how do I find the acceleration)? Thanking you in advance (sorry for the stupid questions..i am new to orbital mechanics)

thank you @OhioBob. and what about the change in inclination? how do i calculate the deltav for electric propulsion? what are the formulas used? @regex thank you! but mostly i want to know what formulas to use and do the calculations to find this results.

can someone show me how to calculate the deltavs and dry mass of the satellite for an orbit raising to geo from leo wih electric propulsion?