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Coaxial Plasma Thrusters
Several sources have reported a
second mode of operation in Gas-Fed Pulsed Plasma Thrusters (GF-PPTs).
This
mode is accessible at high specific energies and accelerates the
propellant
through a thick stationary discharge region, rather than through a
dense moving
current sheet (snowplow). This so-called plasma deflagration mode
provides
significantly higher thrust efficiency and specific impulse accompanied
by
reduced electrode erosion. Analytical research focuses on developing a
model that
describes this second mode. The theoretical work is supported by
experiments on
our 3 kJ Coaxial High Energy (CHENG) thruster. Results show
similarities to detonations
and deflagrations in combustion science and inspired a model that is
based on
an analogy to the Rankine-Hugoniot theory from combustion theory. The
combustion theory is extended to hydromagnetics and has shown good
agreement
with second mode data. In addition, it also offers new insight to the
snowplow
mode, suggesting that it behaves more like a plasma detonation than an
impermeable sheet.
Related Papers