Development and testing of a vortex-driven, high-regression rate hybrid rocket engine

Development and testing of a vortex-driven, high-regression rate hybrid rocket engine

著者名:

Knuth, W. ( Orbital Technologies Corporation (ORBITEC(TM)) )
Gramer, D. ( Orbital Technologies Corporation (ORBITEC(TM)) )
Chiaverini, M. ( Orbital Technologies Corporation (ORBITEC(TM)) )
Sauer, J. ( Orbital Technologies Corporation (ORBITEC(TM)) )

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:

1998

発行年:

1998

通号:

98-3507

ペーパー番号:

98-3507

開始ページ:

1

終了ページ:

13

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:	ZA00050858
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	34th
会議開催地:	Cleveland, OH
会議開催年:	1998.07.13-1998.07.15
論文注記:	34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 13-15, 1998/Cleveland, OH

類似資料:

1 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	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 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	8 テクニカルペーパー Advanced cryogenic solid hybrid rocket engine developments: concept and testing St.Clair, C., Rice, E., Knuth, W., Gramer, D. American Institute of Aeronautics and Astronautics
3 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	9 テクニカルペーパー Combustion Oscillations in High-Regression-Rate Hybrid Rockets Zilwa, S.D., Karabeyoglu, A., Zilliac, G., King, L., Reinath, M. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Vortex Combustion Chamber Development for Future Liquid Rocket Engine Applications. Chiaverini, M.J., Malecki, M.J., Sauer, J.A., Knuth, W.H. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Scale-Up Tests of High Regression Rate Liquefying Hybrid Rocket Fuels Arif Karabeyoglu, M., Zilliac, G., Cantwell, B., DeZilwa, S., Castellucci, P. American Institute of Aeronautics and Astronautics
5 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	11 テクニカルペーパー MARS ISRU CO/O2 HYBRID ENGINE DEVELOPMENT STATUS Rice, Eric E., Chiaverini, Martin J., Clair, Christopher P. St., Knuth, William H., Gustafson, Robert J. American Institute of Aeronautics and Astronautics
6 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	12 テクニカルペーパー Experimental investigation of a metallized cryogenic hybrid rocket engine Gramer, D., Rice, E., Knuth, W., St.Clair, C. American Institute of Aeronautics and Astronautics

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