// interplanetary transfers

Hohmann Transfer

Two-burn minimum energy transfer between two coplanar circular orbits. The first burn to enter the ellipse, and the second to circularise.

DEPARTURE FROM

Orbit radius 1.000 AU

Orbital velocity —

ARRIVAL TO

Orbit radius 1.524 AU

Orbital velocity —

⚠ select two different orbits

// outputs

Delta V₁

—

km/s

Delta V₂

—

km/s

Total Δv

—

km/s

Travel time

—

days

Semi-major axis —

Eccentricity —

Phase angle —

TRANSFER SIMULATION WAITING

Speed 10x Day 0

CENTRAL BODY

INITIAL ORBIT DEPARTURE

Altitude (km)

Inclination (deg)

Orbital radius —

Orbital velocity —

FINAL ORBIT ARRIVAL

Altitude (km)

Inclination (deg)

Orbital radius —

Orbital velocity —

// outputs

Delta V burn 1

—

m/s

Delta V burn 2

—

m/s

Total Δv

—

m/s

Time of flight

—

min

Inclination Δv —

Transfer semi-major axis —

Eccentricity —

TRANSFER ORBIT WAITING

speed 1× t= 0.0 min