Decomposition Chamber Thermal Characterization Test of an Improved 400N Monopropellant Hydrazine Thruster.

Decomposition Chamber Thermal Characterization Test of an Improved 400N Monopropellant Hydrazine Thruster.

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.:

2002-4283

Paper no.:

2002-4283

Pages:

10

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 Performance Characterization Test for the Ariane 5 Attitude Control System 400 N Thruster. Holzwarth, M., Serbest, E., Rogall, H. American Institute of Aeronautics and Astronautics	7 Technical Paper Immersion Test Apparatus for Studying Monopropellant Decomposition with Various Catalysts. Miller, K.J., Martin, T.N., Edwards, J.M., Heister, S.D., Meyer, S.E. American Institute of Aeronautics and Astronautics
2 Technical Paper Qualification Test for the Ariane 5 Attitude Control System 400N Thruster Holzwarth, M., Serbest, E., Rogall, H. American Institute of Aeronautics and Astronautics	8 Technical Paper Demonstration Testing of a New 4-N Monopropellant Thruster H. Kagawa, D. Goto, K. Kajiwara, F. Ueno American Institute of Aeronautics and Astronautics
3 Technical Paper Confidence Testing of Shell-405 and S-405 Catalysts in a Monopropellant Hydrazine Thruster McRight, P., Popp, C., Pierce, C., Turpin, A., Urbanchock, W., Wilson, M. American Institute of Aeronautics and Astronautics	9 Technical Paper Development and Test of a Miniature Hydrogen Peroxide Monopropellant Thruster C. Scharlemann, M. Schiebl, K. Marhold, M. Tajmar, P. Miotti, C. Kappenstein, Y. Batonneau, R. Brahmi, C. Hunter American Institute of Aeronautics and Astronautics
4 Technical Paper Development of a 400-N hydrazine thruster for ESA's atmospheric reentry demonstrator Rath, M., Schmitz, H.D., Steenborg, M. American Institute of Aeronautics and Astronautics	10 Technical Paper Effects of test chamber ambient pressure on the performance of hydrogen thrusters for solar thermal rockets Landrum, D. Brian, Beard, Robert M., Tucker, Timothy W. American Institute of Aeronautics and Astronautics
5 Technical Paper Demonstration Tests Results for 1 Lbf Long Life Monopropellant Thruster J. Gervasi, M. Marvin, K. Josten, H. Conomos, R. Driscoll American Institute of Aeronautics and Astronautics	11 Technical Paper Demonstration Testing of a Long-Life 5-Lbf (22-N) MR-106L Monopropellant Hydrazine Rocket Engine Assembly Wilson, M. American Institute of Aeronautics and Astronautics
6 Technical Paper Influence of Fuel on Thermal and Catalytic Decompositions of Ionic Liquid Monopropellants Amariei, D., Courtheoux, L., Rossignol, S., Batonneau, Y., Kappenstein, C., Ford, M., Pillet, N. American Institute of Aeronautics and Astronautics	12 Technical Paper Controlled porosity carbides used as hydrazine decomposition catalysts Gobbo-Ferreira, J., Rodrigues, J.A.J., Hinckel, J.N., Migueis, C.E., DaCruz, G.M. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12