Hi everbody,
Can you please help me to convert this formula into linear form.
Where:
= Gravitational parameter of parent body 3530.461 km³/s²
= The altitude of first orbit (100 km in this case)
= The altitude of second orbit (200 km in this case)
= The radius of parent body (600 km in this case).
Thanks in advance.
Can you please help me to convert this formula into linear form.
Where:
Thanks in advance.