[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Jonash et al., 1962 - Google Patents

40. Current Research and Development on Thrust Chambers

Jonash et al., 1962

View HTML
Document ID
611573682517825084
Author
Jonash E
Tomazic W
Publication year
Publication venue
Proceedings of the NASA-university conference on the science and technology of space exploration

External Links

Snippet

A million pounds of thrust for large boosters, a few ounces of thrust for attitude control systems-this is the range in size of thrust chambers that are under development today. Basic operating principles are the same for all sizes. The state of the art, however, is such that …
Continue reading at books.google.com (HTML) (other versions)

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
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling 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
    • 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
    • F02K9/44—Feeding propellants
    • F02K9/46—Feeding propellants using pumps
    • F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
    • 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
    • F02K9/44—Feeding propellants
    • F02K9/56—Control
    • 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
    • F02K9/425—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants propellants
    • 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
    • F02K9/974—Nozzle- linings; Ablative coatings
    • 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
    • F02K9/80—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • 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
    • 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

Similar Documents

Publication Publication Date Title
Harrje Liquid propellant rocket combustion instability
Sutton History of liquid-propellant rocket engines in Russia, formerly the Soviet Union
Goethert High altitude and space simulation testing
Murthy et al. High-speed flight propulsion systems
Edelman et al. Theoretical effects of vitiated air contamination on ground testing of hypersonic airbreathing engines
US3811280A (en) Process of using storable propellant fuels in supersonic combustion ramjets
Tiliakos et al. Development and testing of a nitrous oxide/propane rocket engine
Jonash et al. 40. Current Research and Development on Thrust Chambers
Kawalec et al. Development of Rocket Engine with Continuously Rotating Detonation supplied by Liquid Propellants
COULBERT Selecting cooling techniques for liquid rockets for spacecraft
Pinto et al. Green gelled propellant highly throtteable rocket motor and gas generator technology: status and application
Chehroudi et al. Liquid propellants and combustion: fundamentals and classifications
Summerfield The Liquid Propellant Rocket Engine
Abramson Investigation of Internal Film Cooling of Exhaust Nozzle of a 1000-pound-thrust Liquid-ammonia Liquid-oxygen Rocket
Seifert Twenty-Five Years of Rocket Development
Casiano Extensions to the time lag models for practical application to rocket engine stability design
US3521452A (en) Rocket nozzle cooling
Hefner Review of combustion stability development with storable propellants.
QOUT perience has shown that all nozzles suffer, in varying degrees, losses in performance that re
Conrad Exploring in aerospace rocketry. 7-Liquid propellant rocket systems
Bushnell Mixing and combustion issues in hypersonic air-breathing propulsion
Anderson et al. Heterogeneous reactions in ignition and combustion of solid propellants
Linne Carbon monoxide and oxygen combustion experiments: a demonstration of Mars in situ propellants
Kaplan Selection of a pressurization system for a storable liquid propellant rocket engine
REED et al. Hydrogen/oxygen auxiliary propulsion technology