|Table of Contents|

Engineering data models of performance and mass for ion and Hall electric propulsions(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2022年01期
Page:
1-13
Research Field:
专论与综述
Publishing date:

Info

Title:
Engineering data models of performance and mass for ion and Hall electric propulsions
Author(s):
ZHANG Tianping1; 2; ZHANG Xueer1; LI Xuan1
(1. Science and Technology on Vacuum Technology and Physics Laboratory,Lanzhou Institute of Physics,Lanzhou 730000,China; 2. Key Laboratory of Space Electric Propulsion Technology of Gansu Province,Lanzhou 730000,China)
Keywords:
performance model;  mass model;  ion electric propulsion;  Hall electric propulsion;  engineering data
PACS:
V439
DOI:
-
Abstract:
In order to provide a general comparative analysis method for selecting ion or Hall electric propulsion(EP)in the design of aerospace missions,empirical models of performance and mass were established for the EP components based on engineering data. The EP components include thrusters,power processing units,thruster selection units,control units,propellant tanks,pressure regulating units,flow rate units,thruster support mechanisms,cables,and pipelines. Based on these component models,an empirical model of dry mass for the EP system was established. The parameters for this system model include thruster power,the number of thrusters,and propellant mass. The performances and benefits of ion and Hall EP were compared using the system model. The results show the necessity of selecting the EP type with respect to a specific mission.

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Last Update: 1900-01-01