← Rocket Science from Scratch (Level 7)
CAPSTONE
Rocket Forge
IDEAL Δv (live)
10986
m/s (losses subtracted)
EST. PAYLOAD TO ORBIT
3000
kg (from full sim)
MAX ALTITUDE
--
km
MAX-Q
--
kPa
TOTAL Δv (sim)
--
m/s achieved
VEHICLE CONFIG
PAYLOAD MASS (kg)
Stage 1
Dry: kg
Prop: kg
Thrust: N
Isp Vac: s
Stage 2
Dry: kg
Prop: kg
Thrust: N
Isp Vac: s
PROPULSION (LIVE FROM NOZZLE LAB)
Isp Vac: 319 s
pc
tc
gamma
molWt
epsilon
These feed Isp/CF into the trajectory model in real time.
AERODYNAMICS (LIVE FROM AIRFOIL LAB)
Cd ≈ 0.27 (derived) | Ref Area 18 m²
Adjust airfoil params below to see drag impact on trajectory instantly.
Camber
AR
Thickness
TRAJECTORY (RK4 integration)
Click "Run Mission" to simulate trajectory
COMPARE TO REAL VEHICLES
RK4 integrator • Pulls live Isp from Nozzle Lab controls • Cd derived from Airfoil Lab • Full architecture defined in Phase 2.5. This is a working v1 tying all previous simulators together.