please hell You may use the text Introduction to Space Flight and the Coordinate Systems handout. 1. (30) Consider a fast transfer from an inner circular orbit of radius n = 1x107m. to an outer ci...
You may use the text Introduction to Space Flight and the Coordinate Systems handout. 1. (30) Consider a fast transfer from an inner circular orbit of radius n = 1x107m. to an outer circular orbit of radius r2-2x10 m. The trajectory has a departure elevation angle of 0 degrees (perigee) and crosses the outer orbit with a true anomaly v. (a) Find the time of flight from perigee (v 0) tov (b) Find the time of flight from perigee (v-)o transfer (ε = (n-n)( n-r2cosv))
You may use the text Introduction to Space Flight and the Coordinate Systems handout. 1. (30) Consider a fast transfer from an inner circular orbit of radius n = 1x107m. to an outer circular orbit of radius r2-2x10 m. The trajectory has a departure elevation angle of 0 degrees (perigee) and crosses the outer orbit with a true anomaly v. (a) Find the time of flight from perigee (v 0) tov (b) Find the time of flight from perigee (v-)o transfer (ε = (n-n)( n-r2cosv))