Declared in FuelInterconnect
Declaration
[Unit("s")]
[Range(0, 1.7976931348623157E+308)]
double SpecificImpulse;Description
Effective specific impulse (seconds) used to convert vent mass flow to thrust when fuel vents to space. Thrust magnitude is Isp * EffectiveFlowRate * g0 (same convention as cold-gas thrusters). Direction: exhaust leaves along the interconnect’s local axis; reaction force on the body is the opposite of the exhaust direction. When zero, venting still removes mass but produces no thrust.