1989
DOI: 10.1016/s1474-6670(17)53410-2
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A Continuous Proportional Low-Thrust Propulsion System

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1989
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Cited by 3 publications
(1 citation statement)
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“…He developed a thrust stand with sub-dyne resolution and demonstrated a specific impulse of 130 s (c=1300 m s −1 ) with an accuracy of about 1%; see figure 1. This parameter was independently verified in later tests [10][11][12].…”
Section: Thruster Design Evolutionmentioning
confidence: 72%
“…He developed a thrust stand with sub-dyne resolution and demonstrated a specific impulse of 130 s (c=1300 m s −1 ) with an accuracy of about 1%; see figure 1. This parameter was independently verified in later tests [10][11][12].…”
Section: Thruster Design Evolutionmentioning
confidence: 72%