Test Facility Development for the 15,000 lb Thrust Peregrine Hybrid Sounding Rocket

Test Facility Development for the 15,000 lb Thrust Peregrine Hybrid Sounding Rocket

Author(s):

Z. Dunn ( Stanford University, Stanford, CA )

G. Zilliac ( NASA Ames Research Center, Moffett Field, CA )

A. Karabeyoglu ( Space Propulsion Group, Sunnyvale, CA )

B. Cantwell ( Stanford University, Stanford, CA )

4 more

Publication title:

AIAA meeting papers on disc

Title of ser.:

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

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-5358

Paper no.:

AIAA Paper 2007-5358

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200717 [CD-ROM 2007 Disc 17]

Type:

Technical Paper

Details

TDL ID:	ZA00049509
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	43rd
Conf. info. (Venue):	Cincinnati, OH
Conf. info. (Date):	2007.07.08-2007.07.11
Note for article:	43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, OH, July 8-11, 2007

Similar Items:

1 Technical Paper Design and Development of a 100km Nitrous Oxide/Paraffin Hybrid Rocket Vehicle J. Dyer, E. Doran, Z. Dunn, K. Lohner, C. Bayart, A. Sadhwani, G. Zilliac, B. Cantwel, A. Karabeyoglu American Institute of Aeronautics and Astronautics	7 Technical Paper Modeling Feed System Flow Physics for Self-Pressurizing Propellants J. Dyer, G. Zilliac, A. Sadhwani, A. Karabeyoglu, B. Cantwell American Institute of Aeronautics and Astronautics
2 Technical Paper Status Update for the Peregrine 100km Sounding Rocket Project J. Dyer, E. Doran, M. Marzoña, K. Lohner, E. Karlik, G. Zilliac, B. Cantwell, A. Karabeyoglu American Institute of Aeronautics and Astronautics	8 Technical Paper Fuel Regression Rate Characterization Using a Laboratory Scale Nitrous Oxide Hybrid Propulsion System K. Lohner, J. Dyer, E. Doran, Z. Dunn, G. Zilliac American Institute of Aeronautics and Astronautics
3 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	9 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
4 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	10 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
5 Technical Paper Design and Development of a Sub-Scale Nitrous Oxide Monopropellant Gas Generator K. Lohner, J. Dyer, E. Doran, Z. Dunn, B. Krieger, V. Decker, E. Wooley, A. Sadhwani, B. Cantwell, T. Kenny American Institute of Aeronautics and Astronautics	11 Technical Paper Hybrid Rocket Fuel Regression Rate Data and Modeling G. Zilliac, M. Karabeyoglu American Institute of Aeronautics and Astronautics
6 Technical Paper 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	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