|Table of Contents|

Overview of nuclear thermal propulsion technologies(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2011年04期
Page:
1-11
Research Field:
专论与综述
Publishing date:

Info

Title:
Overview of nuclear thermal propulsion technologies
Author(s):
LIAO Hong-tu
Shanghai Institute of Space Propulsion, Shanghai 200233, China
Keywords:
nuclear thermal propulsion technical approach space application de
PACS:
V439.5-34
DOI:
-
Abstract:
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.

References:

[1]MIKE W. Marshall space flight center and the reactor-in-flight stage: a look back at using nuclear propulsion to power space vehicles in the 1960's,AIAA-2003-4588[R]. USA: AIAA, 2003.
[2]GUNN S V, EHRESMAN C M. The space propulsion technology base established four decades ago for the thermal nuclear rocket is ready for current application,AIAA 2003-4590[R]. USA: AIAA, 2003.
[3]CHARLES E W. Cycle trades for nuclear thermal rocket propulsion systems,AIAA 2003-5131[R]. USA: AIAA, 2003.
[4]RUSSELL C, JOSEPH J, ROBERT B F, et al. TRITON: a trimodal capable, thrust optimized nuclear propulsion and power system for advanced space missions,AIAA 2004-3863[R]. USA: AIAA, 2004.
[5]BULMAN M J, NEILL T M, STANLEY K B. LANTR engine system integration,AIAA 2004-3864[R]. USA: AIAA, 2004.
[6]WILLIAM J C, JEFFERY A H. Current status of hot hydrogen test facilities at BWXT to support future nuclear propulsion research and development,AIAA 2004-3867[R]. USA: AIAA, 2004.
[7]WILLIAM J C. Review of nuclear fuel options for NEP and bi-modal concept,AIAA 2004-4230[R]. USA: AIAA, 2004.
[8]Anon. The role of nuclear power and nuclear propulsion in the peaceful exploration of space[M]. Vienna: International Atomic Energy Agency, 2005.
[9]POWELL J, GEORGE M, JOHN P. Nuclear propulsion and power systems for near term exploration of the solar system, AIAA 2005-2597[R]. USA: AIAA, 2005.
[10]STEVEN D H. Identification of archived design information for small class nuclear rocket, AIAA 2005-3762 [R]. USA: AIAA, 2005.
[11]MICHAEL R W. Ground test facility for propulsion and power modes of nuclear engine operation, AIAA 2005-3963[R]. USA: AIAA, 2005.
[12]RODNEY L C, ROBERT B S. Dusty plasma based fission fragment nuclear reactor, AIAA2005-4460[R]. USA: AIAA, 2005.
[13]LUKE S C, ROBERT B, RAVI P. Nuclear gas turbine propulsion system for a long endurance titan aerial vehicle AIAA 2005-4561[R]. USA: AIAA, 2005.
[14]JOYNER R, ANDREA L, JACLYN C. Multidisciplinary analysis of nuclear thermal propulsion design options for human exploration mission, AIAA 2006-4554[R]. USA: AIAA, 2006.
[15]BULMAN M J. Nuclear propulsion for sustainable lunar exploration, AIAA 2006-4555 [R]. USA: AIAA, 2006.
[16]WAYNE J B, RICHARD O B, HAROLD P G. A programmatic and engineering approach to the development of a nuclear thermal rocket for space exploration, AIAA 2006-5082 [R]. USA: AIAA, 2006.
[17]DENNIS L Y, ROGER X L. A tricarbide foam fuel matrix for nuclear thermal propulsion, AIAA 2006-5086 [R]. USA: AIAA, 2006.
[18]KARL W N, STEVEN P S. Engine system model development for nuclear thermal propulsion, AIAA 2006-5087[R]. USA: AIAA, 2006.
[19]WILLIAM J E, DANIEL R K. Design considerations for the nuclear thermal rocket element environmental simulator (NTREES), AIAA 2006-5270 [R]. USA: AIAA, 2006.
[20]KOROTEEV A S, SON E E. Development nuclear gas core reactor in Russia, AIAA 2007-35 [R]. USA: AIAA, 2007.
[21]JOSHUA A C. Integrate propulsion and power modeling for bimodal nuclear thermal rockets, AIAA 2007-5623 [R]. USA: AIAA, 2007.
[22]MISHAAL N A, JULIEN M A, DANIEL R K, et al. Analysis of a grooved-ring reactor concept for nuclear thermal rocket propulsion, AIAA 2007-5624 [R]. USA: AIAA, 2007.
[23]RON J L, JOHN P F. Long duration hot hydrogen exposure of nuclear thermal rocket materials, AIAA 2007-5625 [R]. USA: AIAA, 2007.
[24]RON J L, JOHN P F. Design of resistively heated thermal hydraulic simulator for nuclear rocket reactor cores, AIAA 2007-5626 [R]. USA: AIAA, 2007.
[25]BRUCE G S, STANLEY K B. Small nuclear rocket engine and stage benchmark model, AIAA 2008-4949 [R]. USA: AIAA, 2008.
[26]STANLEY K B, DAVID R M, THOMAX W P. Nuclear thermal propulsion for human exploration and potential threat mitigation of near earth object, AIAA 2008-5034 [R]. USA: AIAA, 2008.
[27]MISHAAL N A, etc. Analysis of a grooved-ring reactor concept for nuclear thermal rocket propulsion, AIAA 2008-5035 [R]. USA: AIAA, 2008.
[28]ROGER D L. Powering space exploration: U.S. space nuclear power, public perceptions, and outer planetary probes, AIAA 2008-5638 [R]. USA: AIAA, 2008.
[29]BULMAN M J. Aerojet nuclear propulsion: enabling future mission, AIAA-2009-5236 [R]. USA: AIAA, 2009.
[30]SCHNITZLER B, BOROWSKI S. An overview of nuclear thermal propulsion graphite, composite, and CERMET designs for thrust sizes 10,000 to 250,000- pounds, AIAA-2009-5237 [R]. USA: AIAA, 2009.

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