[go: up one dir, main page]

Bruckner, 1998 - Google Patents

The ram accelerator: overview and state of the art

Bruckner, 1998

Document ID
16237973327016731895
Author
Bruckner A
Publication year
Publication venue
Ram Accelerators: Proceedings of the Third International Workshop on Ram Accelerators Held in Sendai, Japan, 16–18 July 1997

External Links

Snippet

A new launcher technology called the ram accelerator has been under development since 1983 for applications as a scalable hypervelocity accelerator capable, in principle, of launching projectiles at velocities of 8 km/s or greater. The device is based on an in-bore …
Continue reading at link.springer.com (other versions)

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • 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
    • F02K9/62Combustion or thrust chambers
    • 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
    • F42B10/60Steering arrangements
    • 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
    • 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
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • 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
    • F02K9/80Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/88Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles

Similar Documents

Publication Publication Date Title
Waltrup et al. History of US Navy ramjet, scramjet, and mixed-cycle propulsion development
Hertzberg et al. Ram accelerator-A new chemical method for accelerating projectilesto ultrahigh velocities
US4938112A (en) Apparatus and method for the acceleration of projectiles to hypervelocities
US5853143A (en) Airbreathing propulsion assisted flight vehicle
US9567107B2 (en) Gas gun launcher
US3252281A (en) Rocket system and method
Eidelman et al. Pulse Detonation Engine-A status review and technology development road map
US5485787A (en) Gas gun launched scramjet test projectile
Bruckner The ram accelerator: overview and state of the art
Kailasanath Applications of detonations to propulsion-A review
US3011406A (en) Missile launching system
Bruckner et al. Applications of the ram accelerator to hypervelocity aerothermodynamic testing
Waltrup et al. History of US Navy ramjet, scramjet, and mixed-cycle propulsion development
Bruckner The ram accelerator-A technology overview
Kaloupis et al. The ram accelerator-A chemically driven mass launcher
Knowlen et al. Direct space launch using ram accelerator technology
Bolonkin Hypersonic gas-rocket launch system
Bruckner et al. The ram accelerator: review of experimental research activities in the US
RU144872U1 (en) GAS-DYNAMIC ACCELERATOR OF SOLID BODIES
Knowlen et al. Ram accelerator as an impulsive space launcher: Assessment of technical risks
Yalçın Detonative Rocket-Based Combined Cycle Engine Applications for SSTO Missions: A Comparative Review of Propulsion Technologies, Sustainability, and Performance Metrics
Božić et al. Aerothermal and flight mechanic considerations by development of small launchers for low orbit payloads started from Lorentz rail accelerator
Jaafar et al. Development of solid rocket propulsion system at UTM
Wilbur et al. The electrothermal ramjet
Grosse et al. Development of a Hybrid Rocket Motor Using a Diaphragm for a Small Test Rocket