TECHNIQUES FOR SPECTROSCOPIC MEASUREMENTS IN AN ARCJET NOZZLE

被引：6

作者：

ZUBE, DM ^{[1
]}

MYERS, RM ^{[1
]}

机构：

[1] NASA,LEWIS RES CTR,CLEVELAND,OH 44135

来源：

JOURNAL OF PROPULSION AND POWER | 1992年 / 8卷 / 01期

关键词：

D O I：

10.2514/3.23470

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

ALOW-power laboratory model arcjet thruster has been developed as the basis for a satellite flight propulsion system.1‘2 Operating on hydrazine propellant at a power level of 1.2 kW, the arcjet thruster has demonstrated a specific impulse of 500 s, a thrust efficiency of 35%, and 1000 h lifetime which simulates 10 yr of satellite life. © 1992 American Institute of Aeronautics and Astronautics, Inc., All rights reserved.

引用

页码：254 / 256

页数：3