GB2402462B - Method and device for a multiple step rocket - Google Patents

Method and device for a multiple step rocket

Info

Publication number
GB2402462B
GB2402462B GB0309642A GB0309642A GB2402462B GB 2402462 B GB2402462 B GB 2402462B GB 0309642 A GB0309642 A GB 0309642A GB 0309642 A GB0309642 A GB 0309642A GB 2402462 B GB2402462 B GB 2402462B
Authority
GB
United Kingdom
Prior art keywords
multiple step
step rocket
rocket
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
GB0309642A
Other versions
GB2402462A (en
Inventor
Lars Nilsson
Lars Ax
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Saab AB
Original Assignee
Saab AB
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Saab AB filed Critical Saab AB
Priority claimed from PCT/SE2001/002381 external-priority patent/WO2002036955A1/en
Publication of GB2402462A publication Critical patent/GB2402462A/en
Application granted granted Critical
Publication of GB2402462B publication Critical patent/GB2402462B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • 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
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/76—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants
    • F02K9/763—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants with solid propellant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • 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
    • F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic
    • F05D2250/232—Three-dimensional prismatic conical
GB0309642A 2000-10-31 2001-10-30 Method and device for a multiple step rocket Expired - Lifetime GB2402462B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE0039636 2000-10-31
PCT/SE2001/002381 WO2002036955A1 (en) 2000-10-31 2001-10-30 Method and device for a multiple step rocket

Publications (2)

Publication Number Publication Date
GB2402462A GB2402462A (en) 2004-12-08
GB2402462B true GB2402462B (en) 2005-08-31

Family

ID=33448609

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0309642A Expired - Lifetime GB2402462B (en) 2000-10-31 2001-10-30 Method and device for a multiple step rocket

Country Status (1)

Country Link
GB (1) GB2402462B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103122807A (en) * 2013-01-16 2013-05-29 西北工业大学 Multichannel solid rocket engine ignition sequence control method

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2724237A (en) * 1946-03-05 1955-11-22 Clarence N Hickman Rocket projectile having discrete flight initiating and sustaining chambers
US3385063A (en) * 1962-03-19 1968-05-28 Air Force Usa Multi-stage solid propellant motor
DE1298369B (en) * 1966-07-30 1969-06-26 Messerschmitt Boelkow Blohm Multi-stage solid rocket
US4198896A (en) * 1976-12-28 1980-04-22 Societe Nationale Des Poudres Et Explosifs Self-propelled engine with separable stages
US4745861A (en) * 1985-10-31 1988-05-24 British Aerospace Plc Missiles
WO2000034731A2 (en) * 1998-11-12 2000-06-15 Cordant Technologies, Inc. Gas generating eject motor

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2724237A (en) * 1946-03-05 1955-11-22 Clarence N Hickman Rocket projectile having discrete flight initiating and sustaining chambers
US3385063A (en) * 1962-03-19 1968-05-28 Air Force Usa Multi-stage solid propellant motor
DE1298369B (en) * 1966-07-30 1969-06-26 Messerschmitt Boelkow Blohm Multi-stage solid rocket
US4198896A (en) * 1976-12-28 1980-04-22 Societe Nationale Des Poudres Et Explosifs Self-propelled engine with separable stages
US4745861A (en) * 1985-10-31 1988-05-24 British Aerospace Plc Missiles
WO2000034731A2 (en) * 1998-11-12 2000-06-15 Cordant Technologies, Inc. Gas generating eject motor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103122807A (en) * 2013-01-16 2013-05-29 西北工业大学 Multichannel solid rocket engine ignition sequence control method

Also Published As

Publication number Publication date
GB2402462A (en) 2004-12-08

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Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Expiry date: 20211029