[go: up one dir, main page]

Grosse et al., 2008 - Google Patents

Development of a Hybrid Rocket Motor Using a Diaphragm for a Small Test Rocket

Grosse et al., 2008

Document ID
16346732444254533541
Author
Grosse M
Schlatzke G
Publication year
Publication venue
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit

External Links

Snippet

Hybrid propulsion promises some interesting features for future tactical missile applications in comparison to the normally used solid rocket propulsion:− Real-time thrust control (a thrust modulation ratio of 1: 10 was demonstrated by the HAST aerial target [1]) as required …
Continue reading at arc.aiaa.org (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
    • F02K9/42Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/56Control
    • F02K9/58Propellant feed valves
    • 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
    • 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
    • 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
    • F02K9/24Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges
    • 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
    • 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
    • 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

Similar Documents

Publication Publication Date Title
Waltrup et al. History of US Navy ramjet, scramjet, and mixed-cycle propulsion development
Huang et al. Performance study of a water ramjet engine
Okninski et al. Rocket rotating detonation engine flight demonstrator
Werling et al. Nitrous oxide fuels blends: research on premixed monopropellants at the german aerospace center (DLR) since 2014
Kawalec et al. Development of a liquid-propellant rocket powered by a rotating detonation engine
Feodosiev et al. Introduction to rocket technology
Coleman Overview of pulse detonation propulsion technology
Božić et al. Program AHRES and its contribution to assess features and current limitations of hybrid rocket propulsion
Grosse et al. Development of a Hybrid Rocket Motor Using a Diaphragm for a Small Test Rocket
Naumann et al. Gelled green propellant rocket motor and gas generator technology at bayern-chemie-status and applications for space systems
Bach et al. Development of a Liduid-Propellant Student Sounding Rocket
RU187155U1 (en) Liquid-free rocket engine gasless steam chamber
Pinto et al. Green gelled propellant highly throtteable rocket motor and gas generator technology: status and application
Tokudome et al. An experimental study of a nitrous oxide/ethanol (NOEL) propulsion system
Eilers et al. Regeneratively Cooled Multiple-Use Plug Hybrid for Nanosatellites
Bzdyk et al. Investigation of the operating parameters and performance of an autophage, hybrid rocket propulsion system
Kara et al. Ignition Capability of CO 2 in Hybrid Rockets for Mars Ascent Vehicles
Waxman et al. Paraffin and Nitrous Oxide Hybrid Rocket as a Mars Ascent Vehicle Demonstrator
Stoffel Experimental and theoretical investigation of aerospike nozzles in a hybrid rocket propulsion system
Coma Busquets Specification, design and development of a solid rocket engine for suborbital sounding missions
Pillai Space-capable sounding rocket design for collegiate teams
Humbert et al. Development of Solid Rocket Igniter System for Turn-Key Space Access
Martinez et al. Design of a solid fuel Ramjet Ground launch demonstrator
Satyaprasad et al. Missile propulsion systems
Paccagnella et al. Development of a LOX/Ethanol Gas Generator for a Hybrid-Motor-Based Mini-Launcher