METHOD OF LIQUID FUEL COMPONENTS ENERGETICS INCREASING FOR CARRIER-ROCKETS WITH LIQUID ROCKER ENGINES AND A DEVICE FOR THE METHOD REALIZATION Russian patent published in 2012 - IPC F02K9/42 

Abstract RU 2442010 C2

FIELD: rocket technology.

SUBSTANCE: invention is related to the space-rocket machinery, particularly to the carrier-rockets and upper-stages with the liquid rocket engines. The method of liquid fuel components energetics increasing for carrier-rockets with liquid rocket engines is based on the metal additives and metal compounds input to the fuel. The electric valve activates while starting of the propulsion system, then the blowing gas from the balloon ball comes through the abridger to the press tank that contains a compound of the metal aluminum or the component which was chose from the light metal containing hydride group. The compound comes to the fuel manifold ahead of the propulsion system section through the dosing and mixing system. The device for this method realization contains: fuel tanks, propulsion system, additionally a balloon-ball with the pressed blowing gas. This balloon-ball is connected to the press tank through the electric valve and abridger. The press tank contains compound, dosing and mixing system and is connected to the fuel manifold ahead of the propulsion system section.

EFFECT: increasing of liquid fuel components energetics.

2 cl, 3 dwg

Similar patents RU2442010C2

Title Year Author Number
WITHDRAWAL OF CARRIER ROCKET STAGE SEPARATED PART FROM PAYLOAD ORBIT AND DEVICE TO THIS END 2012
  • Trushljakov Valerij Ivanovich
  • Lempert David Borisovich
  • Lesnjak Ivan Jur'Evich
RU2518918C2
METHOD OF DRIVING CARRIER ROCKET SEPARABLE UNIT FROM PAYLOAD ORBIT AND DEVICE TO THIS END 2011
  • Trushljakov Valerij Ivanovich
  • Kudentsev Vladimir Jur'Evich
  • Kazakov Aleksandr Jur'Evich
  • Kurochkin Andrej Sergeevich
  • Lesnjak Ivan Jur'Evich
RU2482034C1
METHOD OF WITHDRAWING ROCKET CARRIER SEPARATED SECTION (RCSS) FROM PAY LOAD ORBIT AND POWER PLANT TO THIS END 2008
  • Shalaj Viktor Vladimirovich
  • Trushljakov Valerij Ivanovich
  • Kudentsov Vladimir Jur'Evich
  • Odintsov Pavel Valentinovich
RU2406856C2
THRUST PULSE OUTPUT SYSTEM 2014
  • Aksamentov Mikhail Jur'Evich
  • Vasil'Ev Valerij Alekseevich
  • Boltov Elisej Aleksandrovich
  • Goleva Tat'Jana Vasil'Evna
  • Kazakov Vladimir Evgen'Evich
  • Makar'Jants Mikhail Viktorovich
  • Popova Ol'Ga Petrovna
  • Stramousov Valerij Aleksandrovich
RU2560645C1
METHOD OF SPACE REFUSE WITHDRAWAL FROM PAYLOAD ORBIT EXPLOITING CARRIER ROCKET SEPARATED PART AND ACCELERATING UNIT, AND DEVICE TO THIS END 2010
  • Trushljakov Valerij Ivanovich
  • Kudentsov Vladimir Jur'Evich
  • Shatrov Jakov Timofeevich
  • Makarov Jurij Nikolaevich
RU2462399C2
SPACECRAFT PROPELLANT TANK PRESSURIZATION SYSTEM 1996
  • Gorelikov V.I.
  • Sarychev L.N.
  • Tsikhotskij V.M.
RU2119082C1
METHOD FOR HEATING COLD HELIUM GAS FOR A TANK PRESSURIZATION SYSTEM AND A DEVICE FOR ITS IMPLEMENTATION 2021
  • Trushliakov Valerii Ivanovich
  • Urbanskii Vladislav Aleksandrovich
RU2788240C1
UNIFIED SMALL-SIZED UPPER STAGE OF PLATFORM CONFIGURATION WITH WIDE-RANGE ORBITAL MANEUVERING 2023
  • Shmatov Dmitrii Pavlovich
  • Ignatov Aleksei Sergeevich
  • Kruzhaev Konstantin Vladimirovich
  • Lymich Sergei Nikolaevich
  • Levin Vasilii Sergeevich
  • Basharina Tatiana Aleksandrovna
  • Chernyshov Danil Alekseevich
  • Provotorov Georgii Sergeevich
  • Levina Anastasiia Vitalevna
  • Glebov Sergei Evgenevich
  • Akolzin Ivan Vasilevich
RU2810340C1
LIQUID-PROPELLANT ROCKET POWER PLANT 1998
  • Katkov R.Eh.
  • Tupitsyn N.N.
RU2148181C1
LOW-THRUST MODULAR ENGINE UNIT 2014
  • Baryshnikov Ruslan Sergeevich
  • Boltov Elisej Aleksandrovich
  • Goleva Tat'Jana Vasil'Evna
  • Kazakov Vladimir Evgen'Evich
  • Makar'Jants Mikhail Viktorovich
  • Popova Ol'Ga Petrovna
RU2563923C1

RU 2 442 010 C2

Authors

Trushljakov Valerij Ivanovich

Kudentsov Vladimir Jur'Evich

Lempert David Borisovich

Dates

2012-02-10Published

2010-02-25Filed