Official Falcon 9 v1.2 Full Thrust parameters.

Falcon9Params¶

@dataclass(frozen=True)
class Falcon9Params:
    m0: float = 549_054.0        # Gross liftoff mass [kg]
    thrust1: float = 7_686_000.0 # Stage 1 thrust [N]
    thrust2: float = 981_000.0   # Stage 2 thrust [N]
    isp1: float = 282.0          # Stage 1 Isp [s]
    isp2: float = 348.0          # Stage 2 Isp [s]
    t2_burn: float = 397.0       # Stage 2 burn time [s]
    m1_dry: float = 22_000.0     # Stage 1 dry mass [kg]
    m2_dry: float = 4_000.0      # Stage 2 dry mass [kg]
    interstage: float = 2_000.0  # Interstage mass [kg]
    diameter: float = 3.7        # Vehicle diameter [m]

Parameter Details¶

Propulsion¶

Mass Budget¶

Aerodynamics¶

Usage¶

from apogee_launch.falcon9 import FALCON9_DEFAULT, Falcon9Params

# Use default
params = FALCON9_DEFAULT

# Custom parameters
custom = Falcon9Params(
    m0=500_000,
    thrust1=7_000_000,
    # ...
)