Proposal of Specific Impulse Prediction Method for Bipropellant Thrusters
نویسندگان
چکیده
منابع مشابه
Comparison study of exhaust plume impingement effects of small mono- and bipropellant thrusters using parallelized DSMC method
A space propulsion system is important for the normal mission operations of a spacecraft by adjusting its attitude and maneuver. Generally, a mono- and a bipropellant thruster have been mainly used for low thrust liquid rocket engines. But as the plume gas expelled from these small thrusters diffuses freely in a vacuum space along all directions, unwanted effects due to the plume collision onto...
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ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
سال: 2020
ISSN: 0549-3811,2189-4205
DOI: 10.2322/tjsass.63.189