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Fluidic pressure regulators
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mangion, C. Miller, W. |
| Copyright Year | 1972 |
| Description | Three basic areas for possible application of fluidic control to rocket engine subsystems were identified and six subsystem configurations were analyzed for study. Results provide indication of tradeoffs involved between conventional and fluidic regulators and should be of interest to control and applications engineers who need to make similar analyses. |
| File Size | 100619 |
| File Format | |
| Language | English |
| Publisher Date | 1972-01-01 |
| Access Restriction | Open |
| Subject Keyword | Propellant Storage Hydrazines Transducers Propulsion System Performance Liquid Rocket Propellants Fluid Flow Rocket Engines Valves Gas Pressure Propellant Tanks Propulsion System Configurations Rare Gases Spacecraft Propulsion Jet Amplifiers Fuel Tank Pressurization Compressed Air Pressure Regulators Fluidics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
