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核火箭原理、发展及应用 被引量:10

The fundamentals, developments and applications of nuclear rocket propulsion
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摘要 人类在不懈地对浩瀚的宇宙进行着探索,而强劲的推力是人类探索宇宙的关键。化学火箭在人类宇宙探索活动中书写了一页又一页的华丽篇章,现今在人类新的探索使命下,出现了激光、太阳能、微波、核热能等新的推进技术。在这些技术中,核火箭推进无疑是人类继续探索太空最有希望的技术之一。对核火箭的原理、发展状况以及应用前景进行了介绍。 The vast space is explored continuously by human being, and the strong thrust is of great importance. The chemical rocket has been used during the former exploration events. Today, some new propulsion technologies, such as laser, solar energy, microwave and nuclear thermal propulsion are presented. In these technologies, one of the most promising technologies for the future exploration to deep space may be Nuclear Thermal Rocket Propulsion. The fundamentals, developments and applications of Nuclear Thermal Rocket Propulsion will be discussed here.
出处 《火箭推进》 CAS 2005年第2期37-43,共7页 Journal of Rocket Propulsion
关键词 核火箭 原理 应用 探索活动 推进技术 火箭推进 发展状况 人类 宇宙 太阳能 推力 太空 nuclear thermal energy rocket engine high temperature gas-cooled reactor
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参考文献10

  • 1[1]John D Cinnamon. Nuclear thermal rocket propulsion (Design Issues and Concepts)[J]. Aerospace Engineering,1992, 396, Spring.
  • 2[2]James R Powell, George Maise , John Paniagua Jon P, John D Metzger , Hui Zhang.Phase1 -final report Lightweight, high specific impulse(1000Sec) Space Propulsion Systems[R].Plus ultra technologies, Inc. Oct 1999.
  • 3[3]A Y Goldin, et al. Development of nuclear engines in the USSR(presented by J R Wetch) [R]. AIAA Paper 1991-3648.
  • 4[4]A C Marshall, J E Brockman, M S Y Chu, et al. Review of gas-cooled reactor concepts for SDI applications [R].Sandia National Laboratories, August 1,1989.
  • 5[5]H Ludewing, J R Powell, M Todosow, G Maise, R Barletta,D G Schweitzer. Design of particle bed reactors for the space nuclear thermal propulsion program[J]. Progress in Nuclear Energy, 1996, Vol 30, No. 1.
  • 6[6]James Powell, John Paniagua,George Maise.MITEE: An ultra lightweight nuclear engine for new and unique planetary science and exploration missions[M]. 1998.
  • 7[7]Samim Anghaie, Travis Knight, Reza Gouw,Eric Furman. Square Lattice Honeycomb tri-carbide fuels for 50 to 250kN variable thrust NTP Design[M]. Innovative Nuclear Space Power and Propulsion Institute (INSPI).2001.
  • 8[8]George Maise,James R Powell,John Paniagua. Exploration of jovian atmosphere using nuclear ramjet flyer[M]. 1998.
  • 9[9]Brice N Cassenti. The promise of nuclear pulse propulsion[R]. AIAA-2000-3362.
  • 10[10]Stanley K Borowski,Leonard A Dudzinski. "2001: a space odyssey" Revisited-The feasibility of 24 hour commuter flights to the moon using NTP propulsion[R]. NASA/TM-1998-208830/REV2, 2003.

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