DOE OSTI · 21428636
Rectangular Pulsed Laser-Electromagnetic Hybrid Accelerator
Abstract
Experimental investigation of impulse-bit and propellant consumption rate, or mass shot, per single pulse discharge was conducted to characterize the thrust performance of the rectangular laser-electromagnetic hybrid acceleration thruster with various propellant materials. From the result, alumina propellant showed significantly superior performance. The largest values of the measured impulse-bit, specific impulse and thrust efficiency were 49 {mu}Nsec, 6,200 sec and 22%, respectively.
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Kishida, Yoshiaki, Katayama, Masahiro, Horisawa, Hideyuki. 2010-10-13. Rectangular Pulsed Laser-Electromagnetic Hybrid Accelerator. https://doi.org/10.1063/1.3508554
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