SOLID-FUEL REGRESSION RATE AND COMBUSTION BEHAVIOR OF VORTEX HYBRID ROCKET ENGINES

SOLID-FUEL REGRESSION RATE AND COMBUSTION BEHAVIOR OF VORTEX HYBRID ROCKET ENGINES

著者名:

Knuth, William H. ( Orbital Technologies Corporation (ORBITEC TM) )
Chiaverini, Martin J.
Gramer, Daniel J.
Sauer, J. Arthur

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:

1999

発行年:

1999

通号:

99-2318

ペーパー番号:

99-2318

開始ページ:

1

終了ページ:

12

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:	ZA00050872
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	35th
会議開催地:	Los Angeles, CA
会議開催年:	1999.06.20-1999.06.23
論文注記:	35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 20-24 June 1999 Los Angeles, California

類似資料:

1 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	7 テクニカルペーパー Regression rate and heat transfer correlations for HTPB/GOX combustion in a hybrid rocket motor Chiaverini, Martin J., Kuo, Kenneth K., Peretz, Arie, Harting, George C. American Institute of Aeronautics and Astronautics
2 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	8 テクニカルペーパー Thermal pyrolysis and combustion of HTPB-based solid fuels for hybrid rocket motor applications Chiaverini, Martin J., Serin, Nadir, Johnson, David K., Lu, Yeu-Cherng, Kuo, Kenneth K., Risha, Grant A. 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 Pyrolysis behavior of hybrid rocket solid fuels under rapid heating conditions Chiaverini, Martin J., Harting, George C., Lu, Yeu-Cherng, Kuo, Kenneth K., Peretz, Arie, Jones, Steve, Wygle, Brian, … American Institute of Aeronautics and Astronautics
4 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	10 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
5 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	11 テクニカルペーパー Premixing rocket engine injectors for high pressure gaseous oxygen and hydrogen Knuth, William H., Gramer, Daniel J., St. Clair, Christopher P. American Institute of Aeronautics and Astronautics
6 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	12 テクニカルペーパー PREMIXING ROCKET ENGINE INJECTORS FOR HIGH PRESSURE GASEOUS OXYGEN AND HYDROGEN Knuth, William H., Gramer, Daniel J., Clair, Christopher P. St. American Institute of Aeronautics and Astronautics

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