Design and use of a batch reactor for catalytic decomposition of different monopropellants

Author:

Eloirdi Rachel1,Rossignol Sylvie1,Chauveau Michael1,Kappenstein Charles1,Duprez Daniel1,Pillet Nicolas2

Affiliation:

1. CNRS, Lab. de Catalyse en Chimie Organique, Poitiers, France

2. CNES, Toulouse, France

Publisher

American Institute of Aeronautics and Astronautics

Reference23 articles.

1. Jankowsky, R.S. "HAN-based Monopropellant Assessment forSpacecraft", AIAA paper 96-2863.

2. Callahan L.W., Curran P.M. and Wickenheiser T.J."On-board Propulsion forCommunications Satellites",AIAA paper96-1142.

3. Morgan O.M. and Meinhardt D.S. "Monopropellant Selection Criteria -Hydrazine and other Options",AIAA Paper 99-2595.

4. Mittendorf D., Facinelli W.and Sarpolus R. "Experimental Development ofa Monopropellant for SpacePropulsion Systems",AIAA paper 97-2951.

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. MONOMETALLIC AND BIMETALLIC PT-BASED NANOPARTICLES AS TETRAMETHYLTETRAZENE (TMTZ) DECOMPOSITION CATALYSTS;International Journal of Energetic Materials and Chemical Propulsion;2018

2. Experimental Characterization of a 5 N Hydrogen Peroxide Monopropellant Thruster Prototype;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

3. Experimental Characterization of Advanced Materials for the Catalytic Decomposition of Hydrogen Peroxide;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

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