During , the remaining rocket has mass and velocity , while the expelled positive mass has velocity to first order. Subtract the initial momentum from their final momentum to obtain . Equating this to the external impulse gives the rocket equationWith and , this reduces to . Therefore, for initial velocity and ,For a launch from rest,The inequality makes the initial upward acceleration positive. Equality gives no upward launch from rest. In the zero-drag limit, . These expressions apply while the prescribed burn law and constant- approximation remain valid.
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