Hohmann Transfer

CENTRAL BODY

Body MassN/A
PeriapsisN/A
ApoapsisN/A
Sphere of InfluenceN/A

ORBIT INPUTS

ROCKET INPUTS

RESULTS

Transfer TypeN/A
Burn 1 (Δv₁)N/A
Burn 2 (Δv₂)N/A
Total (Δv)N/A
Transfer TimeN/A
Propellant MassN/A
Initial MassN/A