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21 changes: 21 additions & 0 deletions src/utilities/simIncludeThruster.py
Original file line number Diff line number Diff line change
Expand Up @@ -473,6 +473,27 @@ def TEST_Thruster(self, TH):

return

#
# NanoAvionics EPSS C2:
#
# Information Source:
# https://satcatalog.s3.amazonaws.com/components/901/SatCatalog_-_NanoAvionics_-_EPSS_C2_-_Datasheet.pdf
# https://www.youtube.com/watch?v=_YOA2swigBw
#
# This is a NanoAvionics EPSS C2 monopropellant thruster
#
def EPSS_C2(self, TH):
# maximum thrust BOL [N]
TH.MaxThrust = 1.0
# minimum thruster on time [s]
TH.MinOnTime = 0.010 # Guesstimate based on similar thrusters & estimate based on minimum impulse
# Isp value [s]
TH.steadyIsp = 230.0 # Figure 5 of datasheet
# nozzle area [m^2]
TH.areaNozzle = 6.0e-7 # [m^2] Guesstimate

return

def Blank_Thruster(self, TH):
# this method doesn't set any thruster properties. Rather, it is assumed that all thruster
# properties are defined explicitly in the create function, or external to the create function
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