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Volumn 62, Issue 6, 2009, Pages 219-224

Advantages of fast ignition scenarios with two hot spots for space propulsion systems

Author keywords

Fast ignition; Nuclear pulse propulsion

Indexed keywords

FAST IGNITION; FAST IGNITION SCENARIO; IN-SPACE PROPULSION; LARGE AMOUNTS; MICRO EXPLOSION; NUCLEAR PULSE PROPULSION; SPACE PROPULSION SYSTEM; THERMONUCLEAR FUELS;

EID: 70349686624     PISSN: 0007084X     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (4)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.