Preparing Launch vehicle
Launch Vehicle
Flight assemblySystems cutaway

01Launch vehicle / LV—01

Thrust,contained.

A launch vehicle is a vertical chain of structures, tanks, guidance and engines aligned around one load path.

Stage
8.8 m
System
12 groups
State
5 engines

02Primary structure / Airframe scan

Skin carriesthe load.

Panel seams, clamp bands and twin side boosters pass aerodynamic and engine loads into the central vehicle shell.

Stage
+Y axis
System
2 boosters
State
3 bands

03Payload fairing / Unlock

Release theload path.

The clamp band unloads first. Six pushers extend in sequence before either fairing half is allowed to move.

Stage
1 band
System
6 pushers
State
Low shock

04Payload fairing / Jettison

Rotate, thenclear.

Port and starboard shells hinge apart with a slight timing offset, twist clear and establish payload clearance.

Stage
2 halves
System
34° hinge
State
Clear

05Payload adapter / Separation

Purpose,released.

The adapter ring unloads, spring force lifts the spacecraft and the avionics deck counter-rotates for inspection.

Stage
Adapter
System
Spring
State
Uplink

06Tank section / Cutaway

Cold mass.Stored energy.

The shell becomes a technical layer while tank domes, pressurant bottles and the oxidizer/fuel volumes separate subtly.

Stage
LOX
System
Fuel
State
Pressure

07Propellant path / Valve sequence

Open. Route.Condition.

Four valves open from tank to engine while staggered pulses trace both downcomers through the thrust structure.

Stage
4 valves
System
2 feeds
State
Chilldown

08Thrust vector / Gimbal check

Five engines.Five vectors.

Each thrust chamber sweeps independently, exposing turbopumps, injector manifolds, actuators and nozzle extensions.

Stage
5 gimbals
System
2 axes
State
Nominal

09Terminal count / Dependency lock

Lock everysystem.

Engines, feed system, tanks, avionics, payload and fairings return in structural order before start permission.

Stage
T−10
System
Locked
State
Go

10Ignition command / Liftoff

One vehicle.Upward.

Bright cores stabilize inside turbulent plumes, shock cells form and the exhaust spreads across the launch datum.

Stage
T−0
System
Stable thrust
State
Liftoff
Vehicle sourceLoading vehicleValidating vehicle contract
Index02
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