Scale-Up Tests of High Regression Rate Liquefying Hybrid Rocket Fuels

Scale-Up Tests of High Regression Rate Liquefying Hybrid Rocket Fuels

Author(s):

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2003

Pub. Year:

2003

No.:

2003-1162

Paper no.:

2003-1162

Pages:

19

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001712
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	41st
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2003.01.06-2003.01.09
Note for article:	41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 6-9 January 2003

Similar Items:

1 Technical Paper Development of Scalable Space-Time Averaged Regression Rate Expressions for Hybrid Rockets Karabeyoglu, A., Cantwell, B., Zilliac, G. American Institute of Aeronautics and Astronautics	7 Technical Paper Nitrous Oxide Hybrid Rocket Motor Fuel Regression Rate Characterization E. Doran, J. Dyer, K. Lohner, Z. Dunn, B. Cantwell, G. Zilliac American Institute of Aeronautics and Astronautics
2 Technical Paper Hybrid Rocket Fuel Regression Rate Data and Modeling G. Zilliac, M. Karabeyoglu American Institute of Aeronautics and Astronautics	8 Technical Paper Dynamic Optimization of a Paraffin-Fueled Hybrid Rocket P. Urbanczyk, B. Cantwell, M. Karabeyoglu American Institute of Aeronautics and Astronautics
3 Technical Paper Development of High-Burning-Rate Hybrid-Rocket-Fuel Flight Demonstrators Karabeyoglu, M.A., Zilliac, G., Castellucci, P., Urbanczyk, P., Stevens, J. American Institute of Aeronautics and Astronautics	9 Technical Paper DEVELOPMENT AND TESTING OF PARAFFIN-BASED HYBRID ROCKET FUELS Karabeyoglu,M.A., Cantwell,B.J., Altman,D. American Institute of Aeronautics and Astronautics
4 Technical Paper Transient Modeling of Hybrid Rocket Low Frequency Instabilities Karabeyoglu, M.A., DeZilwa, S., Cantwell, B.J., Zilliac, G. American Institute of Aeronautics and Astronautics	10 Technical Paper Test Facility Development for the 15,000 lb Thrust Peregrine Hybrid Sounding Rocket Z. Dunn, J. Dyer, K. Lohner, E. Doran, C. Bayart, A. Sadhwani, G. Zilliac, A. Karabeyoglu, B. Cantwell American Institute of Aeronautics and Astronautics
5 Technical Paper 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	11 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
6 Technical Paper Time-Resolved Fuel-Grain Regression Measurement in Hybrid Rockets De Zilwa, S., Zilliac, G., Karabeyoglu, A., Reinath, M. American Institute of Aeronautics and Astronautics	12 Technical Paper Evaluation of the Homologous Series of Normal Alkanes as Hybrid Rocket Fuels Karabeyoglu, A., Cantwell, B., Stevens, J. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12