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Orbital Mechanics
Rocket Mass Ratio in The Two Body Problem Formulas
Rocket Mass Ratio is the ratio of the rocket’s wet mass (vehicle plus contents plus propellant) to its dry mass (vehicle plus contents). And is denoted by M
R
.
Formulas to find Rocket Mass Ratio in The Two Body Problem
f
x
Rocket Mass Ratio
Go
List of variables in The Two Body Problem formulas
f
x
Change in Rocket Velocity
Go
f
x
Rocket Exhaust Velocity
Go
FAQ
What is the Rocket Mass Ratio?
Rocket Mass Ratio is the ratio of the rocket’s wet mass (vehicle plus contents plus propellant) to its dry mass (vehicle plus contents).
Can the Rocket Mass Ratio be negative?
{YesorNo}, the Rocket Mass Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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