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MALXLABS V5 PHYSICS
Rich Purnell Maneuver
Orbital Eccentricity
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PURNELL MANEUVER
Static Planetary Framework
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1. Aborted Return
2. Earth Slingshot
3. Mars Transfer
4. Mars Assist
5. Final Return
Velocity: 0.0 km/s
Trajectory: Stable
Status: Standby
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ORBITAL DYNAMICS
Periapsis Distance Equation
Eccentricity (e):
0.50
Semi-major Axis (a):
100
Orbital Class:
Elliptical (Closed)
Periapsis Distance (rp):
50.0
Active Formula:
rp = a(1 - e)