Properties for individual thrusters.
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Makes a copy of the specified thruster. |
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Disables the specified control parameter. |
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Enables the specified control parameter. |
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Sees if the specified control is enabled. |
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Returns whether or not the control parameters can be set. |
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The engine model. |
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The equivalent on-time percentage is a factor multiplied by the thrust. The thrust is applied continuously throughout the maneuver and is reduced by the percentage. The mass flow rate is likewise reduced. E.g., for an on-time percentage of 75, the acceleration on the spacecraft will be reduced by 25, and only 75% of the fuel will be used. Dimensionless. |
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The thruster name. |
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A thruster direction value. |
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The thruster efficiency. Dimensionless. |
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A user comment. |