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Bistable (latching) solenoid actuated propellant isolation valve
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wichmann, H. Deboi, H. H. |
| Copyright Year | 1979 |
| Description | The design, fabrication, assembly and test of a development configuration bistable (latching) solenoid actuated propellant isolation valve suitable for the control hydrazine and liquid fluorine to an 800 pound thrust rocket engine is described. The valve features a balanced poppet, utilizing metal bellows, a hard poppet/seat interface and a flexure support system for the internal moving components. This support system eliminates sliding surfaces, thereby rendering the valve free of self generated particles. |
| File Size | 3075915 |
| Page Count | 54 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790016181 |
| Archival Resource Key | ark:/13960/t2p60cj3s |
| Language | English |
| Publisher Date | 1979-05-22 |
| Access Restriction | Open |
| Subject Keyword | Mechanical Engineering Fuel Valves Solenoid Valves Bellows Propellant Actuated Instruments Bistable Circuits Liquid Rocket Propellants Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |