Reactor Modeling for Bimodal Nuclear Thermal Rockets

Reactor Modeling for Bimodal Nuclear Thermal Rockets

著者名:

J. Clough ( Dept. of Aerospace Engineering University of Maryland, College Park, MD )
R. Starkey
M. Lewis
T. Lavelle ( NASA Glenn Research Center, Cleveland, OH )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

シリーズ巻号:

2006

発行年:

2006

通号:

2006-4556

ペーパー番号:

AIAA Paper 2006-4556

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200617 [CD-ROM 2006 Disc 17]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047243
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	42nd
会議開催地:	Sacramento, California
会議開催年:	2006.07.09-2006.07.12

類似資料:

1 テクニカルペーパー Integrated Propulsion and Power Modeling for Bimodal Nuclear Thermal Rockets J. Clough, R. Starkey, M. Lewis, T. Lavelle American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Analysis of a Grooved-Ring Reactor Concept for Nuclear Thermal Rocket Propulsion M. Ashemimry, J. Apeloig, D. Kirk, W. Emrich American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Technology Assessment for Manned Mars Exploration Using a ROSETTA Model of a Bimodal Nuclear Thermal Rocket (BNTR) Marcus, L., Way, D., Medlin, M., Sakai, T., Mclntire, J., Olds, J. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Horizontal Launch Vehicle Weight Modeling for Future Lunar Exploration-Class Payloads Scott, C., Starkey, R., Lewis, M. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Nonequilibrium Surface Interactions Ablation Modeling with the Fully Implicit Ablation and Thermal Response Program A. Beerman, M. Lewis, R. Starkey, B. Cybyk American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Aerodynamic Stability of Re-Entry Heat Shield Shapes for a Crew Exploration Vehicle Johnson, J., Starkey, R., Lewis, M. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Design of a Resistively Heated Thermal Hydraulic Simulator for Nuclear Rocket Reactor Cores R. Litchford, J. Foote, N. Ramachandran, S. Anghaie, T. Wang American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Entry Heat Shield Optimization for Mars Return J. Johnson, M. Lewis, R. Starkey American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Technology Assessment for Manned Mars Exploration Using a ROSETTA Model of a Bimodal Nuclear Thermal Rocket (BNTR) Marcus,Leland, Way,David, Medlin,Matt, Sakai,Tadashi, McIntire,James, Olds,John R. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Analysis of Optimal Earth Entry Heat Shield/Trajectory Configurations J. Johnson, M. Lewis, R. Starkey American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Critical Issues in TBCC Modeling Marshall, A., Gupta, A., Lavelle, T., Lewis, M. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Extending the Flight Mach Number of the SR-71 Inlet Colville, J., Starkey, R., Lewis, M. American Institute of Aeronautics and Astronautics

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