rocketPy
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rocketPy
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Example Usage of Simulation
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Index
_
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A
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B
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C
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D
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E
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F
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I
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L
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M
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N
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P
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R
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S
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T
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U
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X
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Y
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Z
_
__add__() (rocketPy.solution.Solution method)
__init__() (rocketPy.solution.Solution method)
__repr__() (rocketPy.solution.Solution method)
A
A_ref (rocketPy.components.Component attribute)
Acrylic (class in rocketPy.materials)
add() (rocketPy.rocket.Rocket method)
Aluminium (class in rocketPy.materials)
angle_between() (in module rocketPy.util)
B
BodyTube (class in rocketPy.components)
C
CA() (rocketPy.rocket.Rocket method)
CD() (rocketPy.rocket.Rocket method)
CD0() (rocketPy.rocket.Rocket method)
CD0_b() (rocketPy.rocket.Rocket method)
CD0_f() (rocketPy.rocket.Rocket method)
CD0_fb() (rocketPy.rocket.Rocket method)
CD_body_alpha() (rocketPy.rocket.Rocket method)
CD_fin_alpha() (rocketPy.rocket.Rocket method)
Cf() (rocketPy.rocket.Rocket method)
CN() (rocketPy.components.ExternalComponent method)
(rocketPy.components.InternalComponent method)
(rocketPy.rocket.Rocket method)
CNa() (rocketPy.components.BodyTube method)
(rocketPy.components.ExternalComponent method)
(rocketPy.components.FinSet method)
(rocketPy.components.NoseCone method)
(rocketPy.components.Transition method)
(rocketPy.rocket.Rocket method)
Component (class in rocketPy.components)
Cylinder (class in rocketPy.components)
D
density (rocketPy.materials.Aluminium attribute)
(rocketPy.materials.Material attribute)
describe() (rocketPy.components.Component method)
(rocketPy.materials.Material method)
(rocketPy.rocket.Rocket method)
DOF() (rocketPy.solution.Solution method)
E
estimate_inertia (rocketPy.components.Component attribute)
estimate_inertia() (rocketPy.components.BodyTube method)
(rocketPy.components.Component method)
(rocketPy.components.Cylinder method)
(rocketPy.components.FinSet method)
(rocketPy.components.NoseCone method)
(rocketPy.components.Transition method)
estimate_mass (rocketPy.components.Component attribute)
estimate_mass() (rocketPy.components.BodyTube method)
(rocketPy.components.Component method)
(rocketPy.components.Cylinder method)
(rocketPy.components.FinSet method)
(rocketPy.components.NoseCone method)
(rocketPy.components.Transition method)
ExternalComponent (class in rocketPy.components)
F
FinSet (class in rocketPy.components)
full_solve() (rocketPy.simulation.Simulation method)
I
I_xx (rocketPy.components.Component attribute)
I_yy (rocketPy.components.Component attribute)
I_zz (rocketPy.components.Component attribute)
inertia_matrix() (rocketPy.rocket.Rocket method)
inertia_xx() (rocketPy.rocket.Rocket method)
inertia_yy() (rocketPy.rocket.Rocket method)
inertia_zz() (rocketPy.rocket.Rocket method)
InternalComponent (class in rocketPy.components)
L
leading_sweep() (rocketPy.components.FinSet method)
length() (rocketPy.rocket.Rocket method)
M
mach_correction() (in module rocketPy.util)
mass (rocketPy.components.Component attribute)
mass() (rocketPy.rocket.Rocket method)
Material (class in rocketPy.materials)
max_temp (rocketPy.materials.Aluminium attribute)
N
name (rocketPy.components.Component attribute)
(rocketPy.materials.Material attribute)
nominal_solve() (rocketPy.simulation.Simulation method)
NoseCone (class in rocketPy.components)
P
Phenolic (class in rocketPy.materials)
PLA (class in rocketPy.materials)
plot() (rocketPy.components.Component method)
(rocketPy.rocket.Rocket method)
plot_cg() (rocketPy.rocket.Rocket method)
plot_coords() (rocketPy.components.BodyTube method)
(rocketPy.components.Component method)
(rocketPy.components.FinSet method)
(rocketPy.components.NoseCone method)
(rocketPy.components.Transition method)
plot_cp() (rocketPy.rocket.Rocket method)
Plywood (class in rocketPy.materials)
Polycarbonate (class in rocketPy.materials)
R
Rocket (class in rocketPy.rocket)
rocketPy (module)
rocketPy.cli (module)
rocketPy.components (module)
rocketPy.materials (module)
rocketPy.rocket (module)
rocketPy.simulation (module)
rocketPy.solution (module)
rocketPy.util (module)
S
set_boat_tail() (rocketPy.rocket.Rocket method)
set_body_tube() (rocketPy.rocket.Rocket method)
set_fins() (rocketPy.rocket.Rocket method)
set_nose_cone() (rocketPy.rocket.Rocket method)
set_position() (rocketPy.components.Component method)
si() (in module rocketPy.util)
Simulation (class in rocketPy.simulation)
sol() (rocketPy.solution.Solution method)
Solution (class in rocketPy.solution)
solve() (rocketPy.simulation.Simulation method)
static_margin() (rocketPy.rocket.Rocket method)
T
t_max() (rocketPy.solution.Solution method)
t_min() (rocketPy.solution.Solution method)
tensile_modulus (rocketPy.materials.Aluminium attribute)
tensile_strength (rocketPy.materials.Aluminium attribute)
Transition (class in rocketPy.components)
U
unit_vector() (in module rocketPy.util)
X
x_ref (rocketPy.components.Component attribute)
xcg() (rocketPy.components.BodyTube method)
(rocketPy.components.Component method)
(rocketPy.components.FinSet method)
(rocketPy.components.NoseCone method)
(rocketPy.components.Transition method)
(rocketPy.rocket.Rocket method)
xcp() (rocketPy.components.BodyTube method)
(rocketPy.components.Component method)
(rocketPy.components.FinSet method)
(rocketPy.components.NoseCone method)
(rocketPy.components.Transition method)
(rocketPy.rocket.Rocket method)
Y
y_ref (rocketPy.components.Component attribute)
ycg() (rocketPy.components.Component method)
Z
z_ref (rocketPy.components.Component attribute)
zcg() (rocketPy.components.Component method)
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