FIELD: rocket equipment.
SUBSTANCE: invention relates to rocket engineering and specifically to a fuel consumption control system. System for combined control of fuel consumption for rocket propulsion system includes sensors of second fuel consumption: oxidizer and fuel, connected through amplifying-conversion device with on-board central computer, made with possibility to supply control signal to control unit of throttles drives, and fiber-optic level gauges connected with onboard central computer. At that, fiber-optic level gauges contain cylindrical pipe with distributed sensor located in it and communicating with controlled fuel tank, wherein the distributed sensor consists of an optical fiber, an optical reflectometer and an actuating element – a float of magnetic material, inside which three rollers are installed.
EFFECT: invention provides higher accuracy of determining level of fuel components in tanks of carrier rocket, which increases power characteristics of propulsion system of carrier rocket.
3 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SIGNAL FEEDER FOR SEPARATION OF STARTING STAGE OF VERTICALLY LAUNCHING AIRCRAFT | 2019 |
|
RU2719799C1 |
| SYSTEM FOR SINGLE-JET AND MULTI-JET 3D PRINTING OF SOLID PROPELLANT CHARGE (TTZ) WITH COMPOSITE SOLID PROPELLANT (STT) FOR A SOLID-PROPELLANT ROCKET ENGINE (SRE) | 2021 |
|
RU2779811C1 |
| THRUST CONTROL DEVICE FOR THE PROPULSION SYSTEMS OF THE SOYUZ-2 AND ANGARA SPACE ROCKETS, BASED ON THE ASSESSMENT OF THE CURRENT VALUES OF THRUST DURING FLIGHT ACCORDING TO TELEMETRIC INFORMATION FOR FALLING SEPARABLE PARTS INTO A GIVEN AREA | 2022 |
|
RU2793861C1 |
| COMBINED METHOD OF CONTROLLING ROCKET ENGINE FUEL CONSUMPTION WITH MULTIPLE INITIATION AND COMBINED SYSTEM OF FUEL CONSUMPTION CONTROL | 2011 |
|
RU2492122C2 |
| METHOD OF CONTROLLING ROCKET FLUID-PROPELLANT ENGINE OPERATION | 2010 |
|
RU2418188C1 |
| METHOD TO REGULATE MODE OF OPERATION OF LIQUID ROCKET PROPULSION SYSTEM | 2012 |
|
RU2499906C1 |
| METHOD OF ROCKET IN-TANK LIQUID-PROPELLANT GASIFICATION AND DEVICE TO THIS END | 2012 |
|
RU2522536C1 |
| METHOD OF OPERATION OF CLOSED CYCLE LIQUID ROCKET ENGINE WITH AFTERBURNING OF OXIDIZING AND REDUCING GENERATOR GASES WITHOUT COMPLETE GASIFICATION AND LIQUID ROCKET ENGINE | 2022 |
|
RU2801019C1 |
| METHOD FOR SIMULATING PROCESS OF COMBUSTION OF PRODUCTS OF GASIFICATION OF LIQUID ROCKET FUEL COMPONENT RESIDUES AND DEVICE THEREFOR | 2015 |
|
RU2588343C1 |
| UNIVERSAL HYDROGEN-OXYGEN ROCKET MODULE | 2015 |
|
RU2585210C1 |
