火箭推进
火箭推進
화전추진
JOURNAL OF ROCKET PROPULSION
2011年
4期
1-11
,共11页
核热推进%技术途径%空间应用%发展历程
覈熱推進%技術途徑%空間應用%髮展歷程
핵열추진%기술도경%공간응용%발전역정
nuclear thermal propulsion%technical approach%space application%development history
分析了核热推进相对于现有传统推进技术的优势，介绍了可能的技术实现途径，重点是目前已经实现的固相核热推进技术，并归纳了有关文献对于固相核热推进技术的空间应用分析结果；介绍了核热推进技术的发展历程，并对当前发展态势进行了分析；最后针对我国发展核热推进技术提出几点考虑。
分析瞭覈熱推進相對于現有傳統推進技術的優勢，介紹瞭可能的技術實現途徑，重點是目前已經實現的固相覈熱推進技術，併歸納瞭有關文獻對于固相覈熱推進技術的空間應用分析結果；介紹瞭覈熱推進技術的髮展歷程，併對噹前髮展態勢進行瞭分析；最後針對我國髮展覈熱推進技術提齣幾點攷慮。
분석료핵열추진상대우현유전통추진기술적우세，개소료가능적기술실현도경，중점시목전이경실현적고상핵열추진기술，병귀납료유관문헌대우고상핵열추진기술적공간응용분석결과；개소료핵열추진기술적발전역정，병대당전발전태세진행료분석；최후침대아국발전핵열추진기술제출궤점고필。
The advantages of nuclear thermal propulsion （NTP） over existing traditional propulsion technologies are analyzed. Some technical approaches which are possible to be realized are presented. The current state-of-the-art technologies of NTP using solid nuclear reactor are introduced emphatically. The space mission analysis results reported by by some articles about solid phase NTD technology are summarized. The current conditions of development are analyzed after introduction on the deevelopment history of NTP. Some suggestions on future development of NTP in China are made.
