FIELD: cosmonautics.
SUBSTANCE: group of inventions relates to space engineering, namely to design of fuel tanks of spacecrafts intended for storage of liquid fuel in rocket engines. Tank comprises a housing with at least one convex rib forming an angular capillary, and an intake opening located on one of these convex ribs. Inner surface of the tank is made hydrophilic. For use of fuel tank is filled with liquid fuel and supercharging gas. Further, fuel is fed into the engine system through the intake opening. At that, fuel moves due to supercharging gas pressure and local pressure drop in angular capillary.
EFFECT: increased efficiency of fuel supply, increased reliability of the tank, increased useful volume.
12 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FUEL TANK AND ITS INTAKE DEVICE | 2016 |
|
RU2657137C2 |
| DEVICE FOR SIMULATION OF HYDRODYNAMIC PROCESSES IN SPACECRAFT FUEL TANK | 2018 |
|
RU2703745C1 |
| FUEL TANK | 2005 |
|
RU2293665C1 |
| DEVICE FOR SELECTION OF FUEL FROM SPACECRAFT TANKS IN ZERO-GRAVITY CONDITIONS | 2015 |
|
RU2610718C1 |
| TEST BENCH FOR SPACECRAFT FUEL TANK EQUIPPED WITH UNIONS FOR SUPPLY OF FUEL AND SUPERCHARGING GAS TO TANK AND IN-TANK INTAKE DEVICE OF CAPILLARY TYPE WITH PHASE-SEPARATING DEVICE | 2023 |
|
RU2835096C1 |
| DEVICE OF FUEL BLEED FROM TANKS OF SPACECRAFTS UNDER ZERO GRAVITY CONDITIONS | 2015 |
|
RU2609546C1 |
| CAPILLARY STORAGE SYSTEM AND WITHDRAWAL OF FLUID IN ROCKET ENGINE OF SPACE OBJECT (2 VERSIONS) | 2014 |
|
RU2584211C2 |
| METHOD FOR PRE-LAUNCH ZERO-GRAVITY INERTIAL SEPARATION OF GAS INCLUSIONS IN THE LIQUID COMPONENT OF FUEL OF THE ORBITAL UNIT (VARIANTS) | 2021 |
|
RU2775946C1 |
| FUEL TANK OF SMALL SPACECRAFT PROPULSION SYSTEM WITH ELASTIC FUEL DISPLACER | 2023 |
|
RU2810826C1 |
| DEVICE FOR FUEL COLLECTION FROM THE VESSEL AIRCRAFT TANK | 2017 |
|
RU2666004C1 |
