def test_new_propellants(self):
card_str = """
oxid N2O4(L) N 2 O 4 wt%=96.5
h,cal=-4676.0 t(k)=298.15
oxid SIO2 SI 1 O 2 wt%=3,5
h,cal=-216000.0 t(k)=298.15 rho.g/cc=1.48
"""
add_new_oxidizer('GelN2O4', card_str)
# ==========
card_str = """
fuel CH6N2(L) C 1 H 6 N 2 wt%=60.00
h,cal=12900.0 t(k)=298.15 rho=.874
fuel AL 1 wt%=40.00
h,cal=0.0 t(k)=298.15 rho=.1
"""
add_new_fuel('MMH_AL', card_str)
C = CEA_Obj(oxName="GelN2O4", fuelName="MMH_AL", fac_CR=None)
IspODE = C.get_Isp(Pc=1850.0, MR=0.7, eps=40.0)
self.assertAlmostEqual(IspODE, 380.83236183365057, places=3)
# ==========
card_str = """
name H2O2(L) H 2 O 2 wt%=100.00
h,cal=-44880.0 t(k)=298.15 rho.g/cc=1.407
"""
add_new_propellant('MyProp', card_str)
C = CEA_Obj(propName="MyProp", fac_CR=None)
IspODE = C.get_Isp(Pc=1850.0, eps=40.0)
self.assertAlmostEqual(IspODE, 189.9709005711723, places=3)
def createPropellant(wt1, wt2, wt3):
card_str = """
name H2O H 2 O 1 wt%={:.1f}
h,kj/mol=-285.8 t(k)=293.15
name Methanol C 1 H 4 O 1 wt%={:.1f}
h,kj/mol=-239.2 t(k)=293.15
name ADN H 4 N 4 O 4 wt%={:.1f}
h,kj/mol=-134.6 t(k)=293.15
""".format(wt1, wt2, wt3)
add_new_propellant("WaterMethanolADN_Mix", card_str)
p1 = round((p / 20) * 19, 1)
p2 = round((p / 20), 1)
WT0 = j
WT1 = k
WT2 = p1
WT3 = p2
# same name runs affoul of memoized cache.
prop_name = "Propellant" # "prop_{0}_{1}_{2}_{3}".format(WT0, WT1, WT2, WT3)
card_str = """
name pbt C 37.33 H 66.73 N 24.89 O 8.48 wt%={0}
h,cal= 36728.486 t(k)=298.15 rho=1.3
name a3 C 2.4 H 4.1 O 3.1 N 1.3 wt%={1}
h,cal= -46358.545 t(k)=298.15 rho=1.38
name an N 1.0 H 4.0 N 1.0 O 3.0 wt%={2}
h,cal= -87332.284 t(k)=298.15 rho=1.725
name kn K 1.0 N 1.0 O 3.0 wt%={3}
h,cal= -118167.824 t(k)=298.15 rho=2.109
""".format(WT0, WT1, WT2, WT3)
add_new_propellant(prop_name, card_str)
C = CEA_Obj(propName=prop_name,
pressure_units='bar',
cstar_units='m/s',
temperature_units='K',
isp_units='N-s/kg')
tem = C.get_Tcomb(Pc=200)
print(prop_name, tem)
from rocketcea.cea_obj import CEA_Obj, add_new_fuel, add_new_oxidizer, add_new_propellant
# ==========
card_str = """
name H2O2(L) H 2 O 2 wt%=100.00
h,cal=-44880.0 t(k)=298.15 rho.g/cc=1.407
"""
add_new_propellant('MyProp', card_str)
C = CEA_Obj(propName="MyProp")
s = C.get_full_cea_output(Pc=250.0, eps=40.0, short_output=1)
print(s)
def bar2psi(bar):
return bar * 14.504
""" define LMP-103S propellant """
card_str = """
name H2O H 2 O 1 wt%=14.0
h,kj/mol=-285.8 t(k)=293.15
name Ammonia N 1 H 3 wt%=4.6
h,kj/mol=-78.46 t(k)=293.15
name Methanol C 1 H 4 O 1 wt%=18.4
h,kj/mol=-239.2 t(k)=293.15
name ADN H 4 N 4 O 4 wt%=63.0
h,kj/mol=-134.6 t(k)=293.15
"""
add_new_propellant("LMP103S", card_str)
""" define AF-M315E propellant """
card_str = """
name H2O H 2 O 1 wt%=11.0
h,kj/mol=-285.8 t(k)=293.15
name HAN H 4 N 2 O 4 wt%=44.5
h,kj/mol=-366.52 t(k)=293.15
name HEHN C 2 H 9 N 3 O 4 wt%=44.5
h,kj/mol=-486.00 t(k)=293.15
"""
add_new_propellant("AFM315E", card_str)
""" define PeroxideWater98 propellant """
card_str = """
name H2O H 2 O 1 wt%=2.0
h,kj/mol=-285.5 t(k)=293.15
name H2O2 H 2 O 2 wt%=98.0
