Gany, 1991 - Google Patents
Analysis of gun-launched, solid fuel ramjet projectilesGany, 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 …
- 239000004449 solid propellant 0 title abstract description 19
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/97—Rocket nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/08—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/10—Shape or structure of solid propellant charges
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies
- Y02T50/67—Relevant aircraft propulsion technologies
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants 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
- F02K7/10—Plants 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
- F02K7/16—Composite ram-jet/turbo-jet engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means 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
- F42B10/02—Stabilising arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, 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 |