Vortex Combustion Chamber Development for Future Liquid Rocket Engine Applications.

Vortex Combustion Chamber Development for Future Liquid Rocket Engine Applications.

著者名:

掲載資料名:

AIAA paper

シリーズ名:

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

シリーズ巻号:

2002

発行年:

2002

通号:

2002-4149

ペーパー番号:

2002-4149

総ページ数:

13

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001704
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	38th
会議開催地:	Indianapolis, IN
会議開催年:	2002.07.07-2002.07.10
論文注記:	38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, Indiana, 7-10 July 2002

類似資料:

1 テクニカルペーパー Development of a LOX/RP-1 Vortex Combustion Cold-Wall Thrust Chamber Assembly. Sauer, J.A., Knuth, W.H., Malecki, M.J., Chiaverini, M.J., Hall, C.D. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Preliminary CFD analysis of the vortex hybrid rocket chamber and nozzle flow field Knuth, William J., Gramer, Daniel J., Chiaverini, Martin J., Sauer, J. Arthur, Whitesands, R. Harold, Dill, Richard A. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Vortex Thrust Chamber Testing and Analysis for O2-H2 Propulsion Applications Chiaverini, M.J., Malecki, M.J., Sauer, J., Knuth, W.H., Gramer, D.J. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Vortex Chamber Flow Field Characterization for Gelled Propellant Combustor Applications Anderson, M.H., Valenzuela, R., Rom, C., Bonazza, R., Chiaverini, M.J. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Development and testing of a vortex-driven, high-regression rate hybrid rocket engine Knuth, W., Gramer, D., Chiaverini, M., Sauer, J. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Thrust Chamber Technology Developments for Future Launch Vehicle Liquid Rocket Engines Immich,H., Kretschmer,J., Preclik,D. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー SOLID-FUEL REGRESSION RATE AND COMBUSTION BEHAVIOR OF VORTEX HYBRID ROCKET ENGINES Knuth, William H., Chiaverini, Martin J., Gramer, Daniel J., Sauer, J. Arthur American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Cold Flow Analysis of a Vortex Chamber Engine for Gelled Propellant Combustor Applications Anderson, M., Rom, C., Chiaverini, M. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Solid-fuel regression rate and combustion behavior of vortex hybrid rocket engines Knuth, William H., Chiaverini, Martin J., Gramer, Daniel J., Sauer, J. Arthur American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Evaluation of Impinging Stream Vortex Chamber Concepts for Liquid Rocket Engine Applications Trinh, H., Kopicz, C., Bullard, B., Michaels, S. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Experimental investigation of a vortex-driven high-regression rate hybrid rocket engine Knuth, William H., Chiaverini, Martin J., Gramer, Daniel J., Sauer, J. Arthur American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Hot Flow Model of the Vortex Cold Wall Liquid Rocket Fang, D., Majdalani, J., Chiaverini, M. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12