Colloid Thruster Propellant Stability After Radiation Exposure

Author:

Ziemer John1,Marrese-Reading Colleen1,Gamero-Castano Manuel2

Affiliation:

1. Jet Propulsion Laboratory

2. Busek Co. Inc.

Publisher

American Institute of Aeronautics and Astronautics

Reference6 articles.

1. Disturbance reduction system: testing technology for precision formation control

2. Electrospray as a Source of Nanoparticles for Efficient Colloid Thrusters

3. Electrochemical Properties of Imidazolium Salt Electrolytes for Electrochemical Capacitor Applications

4. McCracken, D.R. and Rodgers, M.A.J, "A Chemical Investigation of Sodium Iodide/Glycerol Propellant for Colloid Thrustors (chemical decomposition by ionizing radiation)," UKAEC Report, N75-28118,1974.

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1. Analysis of the Electrospray Plume from the EMI-Im Propellant Externally Wetted on a Tungsten Needle;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

2. Colloid Micro-Newton Thruster Development for the ST7-DRS and LISA Missions;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

3. Microthrust Propulsion for the LISA Mission;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26

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