FIELD: astronautics.
SUBSTANCE: invention relates to aerospace engineering. Method for increasing efficiency of aerial, hypersonic, aerospace and space aircrafts, single- and multiple use on liquid hydrocarbon fuel consists in introduction of fullerenes C60, C70, C84 at their concentration (0.1–0.5) % into it.
EFFECT: invention provides higher efficiency of jet engines and power plants on liquid combustors and coolers by introducing non-metallic additives into them, increasing their density.
13 cl, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| GAS TURBINE ENGINE ANNULAR COMBUSTION CHAMBER HEAD | 2009 |
|
RU2452896C2 |
| METHOD OF PROTECTION OF AEROSPACE SYSTEMS AGAINST LASER WEAPONS | 2001 |
|
RU2212364C2 |
| METHOD OF HEAT EMISSION INTENSIFICATION TO HYDROCARBON FUELS AND COOLERS IN ON-GROUND AND MULTIPLE USAGE SPACE POWER INSTALLATIONS | 2002 |
|
RU2289078C2 |
| METHOD TO INCREASE RELIABILITY OF LIQUID-PROPELLANT ENGINE OF EXPENDABLE AND RECOVERABLE APPLICATION | 2002 |
|
RU2287715C2 |
| NOZZLE WITH EXTERNAL COOLING JACKET | 2022 |
|
RU2810865C1 |
| NOZZLE WITH EFFICIENT COOLING JACKET | 2022 |
|
RU2806710C1 |
| METHOD OF ESTIMATION AND MAINTENANCE OF RELIABILITY OF REUSABLE POWER PLANTS WORKING ON HYDROCARBON FUELS AND COOLANTS | 1998 |
|
RU2215671C2 |
| METHOD FOR DETERMINING THE VALUE OF SUPPLIED ELECTROSTATIC STRESS TO THE PAYOFF NEEDLE IN A NEEDLE-NEEDLE ELECTRODE SYSTEM IN A CLOSED VOLUME WITH LIQUID HYDROCARBON FUEL (COOLANT) | 2021 |
|
RU2785251C1 |
| METHOD FOR DETERMINING THE BORDER OF THE BEGINNING OF THE ZONE OF SATURATION WITH ELECTROSTATIC FIELDS WITH A SYSTEM OF ELECTRODES OF THE "NEEDLE-NEEDLE" TYPE IN A CLOSED VOLUME IN THE ENVIRONMENT OF LIQUID HYDROCARBON FUELS (COOLERS) | 2022 |
|
RU2785830C1 |
| NOZZLE | 2008 |
|
RU2388966C1 |
