Determination of Regression Rate in an Ablating Hybrid Rocket Solid Fuel Using a Physics Based Comprehensive Mathematical Model.

Determination of Regression Rate in an Ablating Hybrid Rocket Solid Fuel Using a Physics Based Comprehensive Mathematical Model.

Author(s):

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

2002

Pub. Year:

2002

No.:

2002-3577

Paper no.:

2002-3577

Pages:

7

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001704
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	38th
Conf. info. (Venue):	Indianapolis, IN
Conf. info. (Date):	2002.07.07-2002.07.10
Note for article:	38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, Indiana, 7-10 July 2002

Similar Items:

1 Technical Paper A Physics Based Mathematical Model to Predict the Regression Rate in an Ablating Hybrid Rocket Solid Fuel Akyuzlu,K., Kagoo,R., Antoniou,A. American Institute of Aeronautics and Astronautics	7 Technical Paper Modeling Instabilities due to Coupling of Acoustic and Hydrodynamic Oscillations in Hybrid Rocket Motors K. Akyuzlu American Institute of Aeronautics and Astronautics
2 Technical Paper A Physics Based Comprehensive Mathematical Model to Predict Motor Performance in Hybrid Rocket Propulsion Systems Antoniou, A., Akyuzlu, K. American Institute of Aeronautics and Astronautics	8 Technical Paper Improvements in the measurement of hybrid rocket fuel regression rate using ultrasonic transducers Leahy, Joseph C., Jackson, John W., Jr. American Institute of Aeronautics and Astronautics
3 Technical Paper Hybrid Rocket Fuel Regression Rate Data and Modeling G. Zilliac, M. Karabeyoglu American Institute of Aeronautics and Astronautics	9 Technical Paper Investigation of GAT as a high regression rate hybrid rocket fuel Luchini, C.B., Wynne, P., Hudson, M.K. American Institute of Aeronautics and Astronautics
4 Technical Paper 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 Technical Paper A parametric study of flame propagation in hybrid rocket motors Akyuzlu, K.M., Nguyen, K., Arves, J.P., Jones, H.S. American Institute of Aeronautics and Astronautics
5 Technical Paper 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 Technical Paper Model for Predicting Fuel Regression Rate in Hybrid Rocket Engines D. Greatrix American Institute of Aeronautics and Astronautics
6 Technical Paper Hydrocarbon hybrid rocket fuel regression rate studies Luchini, C.B., Wynne, P., Hudson, M.K., Rooke, S. American Institute of Aeronautics and Astronautics	12 Technical Paper Effects of swirling oxidizer flow on fuel regression rate of hybrid rockets Tamura, T., Yuasa, S., Yamamoto, K. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12