Nothing Special   »   [go: up one dir, main page]

Gany, 1991 - Google Patents

Analysis of gun-launched, solid fuel ramjet projectiles

Gany, 1991

Document ID
13820523141051627753
Author
Gany A
Publication year
Publication venue
International Journal of Energetic Materials and Chemical Propulsion

External Links

Snippet

The feasibility and performance of self-propelled, gun-launched projectiles by means of a solid fuel ramjet (SFRJ) motor is studied. It is demonstrated that the SFRJ can provide remarkable improvement of the projectile performance without changing the weapon itself …
Continue reading at www.dl.begellhouse.com (other versions)

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10Shape or structure of solid propellant charges
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16Composite ram-jet/turbo-jet engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02Stabilising arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78Other construction of jet pipes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants

Similar Documents

Publication Publication Date Title
US4722261A (en) Extendable ram cannon
US4726279A (en) Wake stabilized supersonic combustion ram cannon
Waltrup et al. History of US Navy ramjet, scramjet, and mixed-cycle propulsion development
US4938112A (en) Apparatus and method for the acceleration of projectiles to hypervelocities
US4574700A (en) Solid rocket motor with nozzle containing aromatic amide fibers
US4164904A (en) Tubular projectile
AU699240B2 (en) Airbreathing propulsion assisted gun-launched projectiles
Webster Liquid fueled integral rocket/ramjet technology review
CN111188697B (en) Solid rocket engine for electromagnetic ejection
Mady et al. Combustion behavior of solid-fuel ramjets
US2946261A (en) Peripheral nozzle spinner rocket
Naumann et al. Double-pulse solid rocket motor technology-applications and technical solutions
Gany Analysis of gun-launched, solid fuel ramjet projectiles
Thomas et al. Addressing emerging tactical missile propulsion challenges with the solid propellant air-turbo-rocket
US5544586A (en) Solid fuel ramjet tubular projectile
US4170875A (en) Caseless rocket design
Bolonkin Hypersonic gas-rocket launch system
Projectiles ALON GANY
Pelosi-Pinhas et al. Solid-fuel ramjet regulation by means of an air-division valve
CN114352437A (en) Solid fuel stamping combined engine suitable for wide Mach number flight
US11655055B2 (en) System and method for aerodynamic drag reduction in airborne systems and vehicles
Limage Solid fuel ducted rockets for ramjet/scramjet missile applications
Dahl et al. Demonstration of solid propellant pulse motor technologies
Krishnan et al. Design and control of solid-fuel ramjet for pseudovacuum trajectories
McFillin Jr et al. Dual-chamber rocket motor operating characteristics