Liquid annular reactor system (LARS) for deep space exploration

Acta Astronautica

Volumn 44, Issue 2, 1999, Pages 167-174

  Maise, George ^a   Paniagua, John ^a   Powell, James R ^a   Ludewig, Hans ^b   Todosow, Michael ^b  

^a Ultra Technologies Inc   (United States)

^b BROOKHAVEN NATIONAL LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTAINMENT VESSELS; FUSION REACTORS; HYDROGEN; LIQUID PROPELLANTS; NUCLEAR FUEL ELEMENTS; ROCKETS; SPACE PROBES; SPACE RESEARCH;

DEEP SPACE EXPLORATION; HYDROGEN PROPELLANT; LIQUID ANNULAR REACTOR SYSTEM;

SPACECRAFT PROPULSION;

EID: 0032642872     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(99)00044-2     Document Type: Article

References (5)

1. A. V. Grosse High-temperature research, Science, vol. 140, pp 781-789, 1963.
2. E.Y.H. Keng and C. Orr, Jr. Investigation of Radiant Heat Transfer to Particle-Seeded Gases for Application to Nuclear Rocket Engine Design, NACA CR-953, Georgia Institute of Technology, Atlanta, GA, USA, 1967.
3. J.R. Williams, et al Thermal radiation absorption by particle-seeded gases, J. Spacecraft, vol. 8, pp 339-346, 1971.
4. A. Friedlander, et al MULIMP software presentation and demonstration, Science Applications International Corporation Presentation to NASA MSFC, 15 December, 1988.
5. S. Isakowitz (Editor) International Reference Guide to Space Launch Systems, 2nd Ed., AIAA, Wash, D.C., 1995.