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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2011
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Article
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Tab 5
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Review Article
Development of Electric and Chemical Microthrusters
Table 5
Performance parameters of the monopropellant thruster system.
Thrust
100–1,500 mN
Specific impulse
140–180 s
V
50–300 m·s
Mass flow rate
0.055–0.9 g·s
Lifetime goal
~16 hours