Engine study

Merlin

Falcon 9 and Falcon Heavy engine family. Cycle: gas-generator cycle. Propellants: RP-1 kerosene + liquid oxygen.

Engine visual

Rocket engine test image

This page includes the generated engine-test image for propulsion, combustion, and simulation context.

Engine Details

Vehicle family	Falcon 1, Falcon 9, Falcon Heavy
Use	booster and vacuum upper-stage variants
Fuel	RP-1
Oxidizer	LOX
Study theme	manufacturable reuse and high production cadence

Combustion Study

Public analysis focuses on propellant pair, thermochemistry, chamber pressure class, cooling, turbomachinery architecture, and integration risk. Exact manufacturing recipes and proprietary controls are intentionally excluded.

Powerhead

Pumps, preburners or gas generator, valves, ignition, health monitoring, and start sequence govern reliability.

Chamber and Nozzle

Combustion stability, regenerative cooling, throat erosion, expansion ratio, and plume environment govern performance.

Reuse

Reusable engines need inspection access, thermal margin, data review, and acceptance criteria after each firing.