International Journal of Aerospace Engineering / 2013 / Article / Fig 6

Research Article

Experimental Investigations of a Krypton Stationary Plasma Thruster

Figure 6

ATON A-3 (a) anode efficiency and (b) specific impulse versus Kr anode mass flow rate under  V.
686132.fig.006a
(a)
686132.fig.006b
(b)

We are committed to sharing findings related to COVID-19 as quickly and safely as possible. Any author submitting a COVID-19 paper should notify us at help@hindawi.com to ensure their research is fast-tracked and made available on a preprint server as soon as possible. We will be providing unlimited waivers of publication charges for accepted articles related to COVID-19. Sign up here as a reviewer to help fast-track new submissions.