FR3065202B1 - SPACE PROPELLER - Google Patents

SPACE PROPELLER Download PDF

Info

Publication number
FR3065202B1
FR3065202B1 FR1753331A FR1753331A FR3065202B1 FR 3065202 B1 FR3065202 B1 FR 3065202B1 FR 1753331 A FR1753331 A FR 1753331A FR 1753331 A FR1753331 A FR 1753331A FR 3065202 B1 FR3065202 B1 FR 3065202B1
Authority
FR
France
Prior art keywords
electric
propulsion
chemical
propulsion module
module includes
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1753331A
Other languages
French (fr)
Other versions
FR3065202A1 (en
Inventor
Frederic Masson
Jerome Vila
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Centre National dEtudes Spatiales CNES
Original Assignee
Centre National dEtudes Spatiales CNES
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Centre National dEtudes Spatiales CNES filed Critical Centre National dEtudes Spatiales CNES
Priority to FR1753331A priority Critical patent/FR3065202B1/en
Publication of FR3065202A1 publication Critical patent/FR3065202A1/en
Application granted granted Critical
Publication of FR3065202B1 publication Critical patent/FR3065202B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00—Using plasma to produce a reactive propulsive thrust
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/401—Liquid propellant rocket engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/402—Propellant tanks; Feeding propellants
    • B64G1/4026—Propellant tanks; Feeding propellants providing propellant to propulsion systems of differing type
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/411—Electric propulsion
    • B64G1/413—Ion or plasma engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/425—Power storage
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B17/00—Pumps characterised by combination with, or adaptation to, specific driving engines or motors
    • F04B17/03—Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by electric motors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B23/00—Pumping installations or systems
    • F04B23/04—Combinations of two or more pumps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/105—Space science
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1078—Maintenance satellites

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

Un système de propulsion spatiale hybride chimique-électrique comprenant une module de propulsion chimique et un module de propulsion électrique. Le module de propulsion chimique comprend une électropompe configurée pour pomper un carburant et/ou un comburant dans une chambre de combustion et le module de propulsion électrique comprend un système d'alimentation électrique pour ioniser et éjecter des atomes d'une masse propulsive. L'électropompe est connectée au système d'alimentation électrique pour être alimentée en énergie électrique. L'invention est d'intérêt pour tous les acteurs actifs dans le domaine de la propulsion spatiale. Le système proposé permet d'optimiser la performance mission (durée et masse de charge utile) d'un étage orbital ou d'un étage supérieur de lanceur, cela au prix d'une complexité système limitée (grâce à la liaison entre baie propulsive chimique et électrique).A chemical-electric hybrid space propulsion system comprising a chemical propulsion module and an electric propulsion module. The chemical propulsion module includes an electric pump configured to pump fuel and / or oxidizer into a combustion chamber and the electric propulsion module includes an electric power system for ionizing and ejecting atoms from a propellant mass. The electric pump is connected to the electrical supply system to be supplied with electrical energy. The invention is of interest to all actors active in the field of space propulsion. The proposed system makes it possible to optimize the mission performance (duration and payload mass) of an orbital stage or of an upper stage of a launcher, at the cost of a limited system complexity (thanks to the connection between the chemical propulsion bay and electric).

FR1753331A 2017-04-18 2017-04-18 SPACE PROPELLER Active FR3065202B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1753331A FR3065202B1 (en) 2017-04-18 2017-04-18 SPACE PROPELLER

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1753331 2017-04-18
FR1753331A FR3065202B1 (en) 2017-04-18 2017-04-18 SPACE PROPELLER

Publications (2)

Publication Number Publication Date
FR3065202A1 FR3065202A1 (en) 2018-10-19
FR3065202B1 true FR3065202B1 (en) 2020-07-17

Family

ID=59930416

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1753331A Active FR3065202B1 (en) 2017-04-18 2017-04-18 SPACE PROPELLER

Country Status (1)

Country Link
FR (1) FR3065202B1 (en)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2636095A1 (en) * 1988-09-05 1990-03-09 Aerospatiale System for supplying the boosters of an artificial satellite with at least one liquid ergol
US9145216B2 (en) * 2011-08-31 2015-09-29 Space Systems/Loral, Llc Unified chemical electric propulsion system
FR2986213B1 (en) * 2012-02-01 2014-10-10 Snecma SPIRAL PROPELLER WITH ELECTRICAL PROPULSION AND CHEMICAL WITH SOLID PROPERGOL
FR2991391B1 (en) * 2012-05-30 2014-07-04 Snecma DEVICE AND METHOD FOR SUPPLYING A PROPULSIVE ENGINE CHAMBER
FR3024436B1 (en) * 2014-07-30 2018-01-05 Safran Aircraft Engines SYSTEM AND METHOD FOR SPACE PROPULSION

Also Published As

Publication number Publication date
FR3065202A1 (en) 2018-10-19

Similar Documents

Publication Publication Date Title
EP3174795B1 (en) Spacecraft propulsion system and method
EP2809582B1 (en) Spacecraft with electrical and chemical solid propulsion
WO2010036291A4 (en) Ionic liquid multi-mode propulsion system
RU2009122187A (en) COMBINED CYCLE MISSION ENGINE
EP2359001B1 (en) Electronegative plasma thruster with optimized injection
FR3043623B1 (en) TERRESTRIAL ELECTRIC VEHICLE FOR PUBLIC TRANSPORT WITH OPTIMIZED ARCHITECTURE.
FR3065202B1 (en) SPACE PROPELLER
WO2022178477A3 (en) Systems and methods for projectile propulsion
Porter et al. Flight qualification of a water electrolysis propulsion system
JP5829095B2 (en) Syringe
RU2476709C1 (en) Liquid propellant rocket engine
RU2455514C1 (en) Multistage booster-rocket, liquid propellant rocket engine and roll nozzle block
EP3636908B1 (en) Rocket engine with turbo pump having a motor-generator
RU2629048C1 (en) Rocket and solid-propellant rocket engine
FR2975441A1 (en) Repressurizing system for use in supply system of rocket engine for repressurizing container containing liquid phase and gas phase of cryogenic propellant, has heating device for reheating cryogenic propellant
RU2273753C1 (en) Simulator of solid-propellant rocket engine for initial phase of operation
RU2538154C1 (en) Solid fuel rocket propulsion system
WO2017023383A1 (en) Liquid fueled pulsed plasma thruster
TWI776218B (en) Motor and fuel-powered hybrid system for rocket thruster
RU2233385C2 (en) Propellant for liquid propellant rocket engines
Wang et al. Numerical investigation on diffusion afterburning of RBCC in ejector mode
Choi Discussions on the Combustion Dynamics of RDE with Relevance to the Liquid Rocket Combustion Instability
RU2230927C2 (en) Solid-propellant rocket engine
RU155042U1 (en) MULTI-CAMERA LIQUID ROCKET ENGINE WITHOUT BURNING THE GENERATOR GAS
Wang et al. Effect of acceleration on the erosion of aft dome insulation of solid motors

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20181019

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8