Regression rate and heat transfer correlations for HTPB/GOX combustion in a hybrid rocket motor

Regression rate and heat transfer correlations for HTPB/GOX combustion in a hybrid rocket motor

著者名:

Chiaverini, Martin J. ( Department of Mechanical Engineering, The Pennsylvania State University )
Kuo, Kenneth K. ( Department of Mechanical Engineering, The Pennsylvania State University )
Peretz, Arie ( Department of Mechanical Engineering, The Pennsylvania State University )
Harting, George C. ( Department of Mechanical Engineering, The Pennsylvania State University )

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:

98-3185

ペーパー番号:

98-3185

開始ページ:

1

終了ページ:

15

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

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6 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	12 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

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