CAM DRIVE SAVINGS

Hohmann Transfer Savings Estimator

Calculate the propellant and cost savings achievable with CAM Drive propellantless technology compared to traditional chemical propulsion systems.

Note: The assumption is the Earth's radius is 6371 km. The mean velocity of a spacecraft is associated with this mean radius.

Input Type:

Initial Orbit (km): (Optional: Used to compute Δv and time if not provided)

Target Orbit (km): (Optional: Used to compute Δv and time if not provided)

Spacecraft Dry Mass (kg): (Mass without propellant)

Specific Impulse (s): (Thruster efficiency; default 300 for chemical)

Fuel Cost per kg ($): (Ballpark for orbital delivery)

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