The concept of a rocket engine using CO2/metal propellants for Mars sample return missions

被引：0
|
作者：
Gökalp, I [1 ]
Shafirovich, E [1 ]
机构：
[1] Federat Rech Energet, CNRS, Lab Combust & Syst Reactifs, F-45071 Orleans 2, France
来源：
THIRD INTERNATIONAL CONFERENCE ON SPACECRAFT PROPULSION | 2000年 / 465卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
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页码：219 / 227
页数：9
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