A projectile is fired from a gun on the ground angled up at 6
degrees.
The gun will give the projectile all of the necesary orbital
velocity.
I need to know the delta-v that a thruster on the projectile would
need for orbit insertion.
a) for a 300km circular orbit
b) for an elliptical orbit with a perigee of 300km, any apogee is
ok.
No inclination change. Initial and final inclination is 15
degrees.
Total projectile mass is 500kg.
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