NEED TO UNDERSTAND SO PLEASE SHOW ALL WORK AND STEPS INCLUDING SKETCHES. WRITE LEGIBLY AND PROVIDE NUMERICAL ANSWER FOR THUMBS UP!! ANSWER ALL PARTS OR LEAVE QUESTION FOR SOMEONE WHO WILL. WILL RATE IMMEDIATELY, THANK YOU!!
An earth satellite is launched into an orbit with the following orbital elements:
i=100 p=10,000km
@=315 e=0.5
What will be the minimum AV (km/s) needed to change this orbit into an equatorial orbit? This AV is accomplished by a single, impulsive maneuver. Hint: it may be helpful to first draw a careful sketch of this orbit, showing the inclination, location of perigee, etc.