人教版高中物理必修2第六章 万有引力与航天3. 万有引力定律教案(2)

人教版高中物理必修2第六章 万有引力与航天3. 万有引力定律导学案

一、航空航天器用电设备及其特性 二、航空航天器的二次能源 三、航空航天器供电系统 四、航空航天供电系统的沿革与发展

Ion Engine and Colloid Thrusters are Electrostatic devices, because the electrostatic forces that accelerate the ions (or droplets) are also directly felt by some electrode, and this is how the structure receives thrust. We could manipulate the expression for thrust density in an ion engine

For a given mass flow m ind thrust F, we would like to minimize the running power

It is well known that rapidly pulsed current tends to concentrate near the surface of copper conductors forming a “skin”. A similar effect occurs when current flows through a highly conductive and rapidly moving plasma: current tends to concentrate near the entrance and exit of the channel. The reason is the appearance of a strong

Colloidal thrusters are electrostatic accelerators of charged liquid droplets. They were first proposed and then intensively studied from around 1960 to 1975 as an alternative to normal ion engines. Their appeal at that time rested with the large “molecular mass” of the droplets, which was known to increase the thrust density of an ion engine

1. Introduction Hall thrusters are electrostatic ion accelerators in which the grid system (which serves in classical ion engines to anchor the negative charges used to accelerate the ions) is replaced with a relatively strong magnetic field perpendicular to the flow

Prof. Manuel Martinez-Sanchez Page 2 of 11Bohm velocity: Why?

JB=Beam ion (and neutralizer electron current) JE=cathode emitted current Jc=ion current to cathode- potential surfaces JD=current through disch. power supply