established · Misc · computed
Rocket thrust controlled by flow rate of ionized combustible gases into combustion chamber
Once gas-ignition occurs, rocket thrust is controlled by the flow rate of the combustible ionized gases entering the combustion chamber of the rocket engine.
Source: The Birth Of New Technology — Rocket Propulsion
Basis
- Confidence
- 0.90
- Recorded
- Published
- 19 Aug 2026
- Device
- Hydrogen Gas Gun
- Component
- combustion-chamber
- Source Ref
- The Birth Of New Technology — Rocket Propulsion
- Notebook Id
- 710
- Source Page Id
- 399
thrust-control flow-rate ignition