Hohmann Transfer
CENTRAL BODY
Earth
Moon
Mercury
Venus
Mars
Jupiter
Saturn
Uranus
Neptune
Custom...
Body Mass
N/A
Periapsis
N/A
Apoapsis
N/A
Sphere of Influence
N/A
Custom Mass
kg
Custom Radius
km
Perihelion
au
Aphelion
au
ORBIT INPUTS
Initial Periapsis (Alt)
km
Initial Apoapsis (Alt)
km
Target Periapsis (Alt)
km
Target Apoapsis (Alt)
km
ROCKET INPUTS
Final Mass
kg
Specific Impulse (Isp)
s
Calculate Transfer
RESULTS
Transfer Type
N/A
Burn 1 (Δv₁)
N/A
Burn 2 (Δv₂)
N/A
Total (Δv)
N/A
Transfer Time
N/A
Propellant Mass
N/A
Initial Mass
N/A
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