TY - GEN
T1 - Modeling of ablation-fed pulsed plasma thruster operation using a new approach to the ablation process
AU - Henrikson, Erik M.
AU - Mikellides, Pavlos
PY - 2008/12/1
Y1 - 2008/12/1
N2 - The magnetohydrodynamics tool MACH2 has been utilized to model an ablation-fed pulsed plasma thruster (APPT) operating at 40, 60, and 80 Joules, corresponding to an experimentally characterized APPT. The ablation process was handled by introducing the propellant mass according to an idealized, quasi-steady, analytic model for Teflon™. This analytic model will be briefly outlined and results of the numerical simulations are presented and discussed. Certain deficiencies in the presented model are identified and addressed with considerations for future improvement.
AB - The magnetohydrodynamics tool MACH2 has been utilized to model an ablation-fed pulsed plasma thruster (APPT) operating at 40, 60, and 80 Joules, corresponding to an experimentally characterized APPT. The ablation process was handled by introducing the propellant mass according to an idealized, quasi-steady, analytic model for Teflon™. This analytic model will be briefly outlined and results of the numerical simulations are presented and discussed. Certain deficiencies in the presented model are identified and addressed with considerations for future improvement.
UR - http://www.scopus.com/inward/record.url?scp=77957851367&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=77957851367&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:77957851367
SN - 9781563479434
T3 - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
BT - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
T2 - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Y2 - 21 July 2008 through 23 July 2008
ER -