GB1120391A - Improvements in or relating to rocketwise propelled projectiles - Google Patents

Improvements in or relating to rocketwise propelled projectiles

Info

Publication number
GB1120391A
GB1120391A GB36558/57A GB3655857A GB1120391A GB 1120391 A GB1120391 A GB 1120391A GB 36558/57 A GB36558/57 A GB 36558/57A GB 3655857 A GB3655857 A GB 3655857A GB 1120391 A GB1120391 A GB 1120391A
Authority
GB
United Kingdom
Prior art keywords
nozzle
booster
charge
sustaining
hot gases
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
Application number
GB36558/57A
Inventor
John William Martin
Reginald John Rosser
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.)
MINI OF TECHNOLOGY
Minister of Technology
Original Assignee
MINI OF TECHNOLOGY
Minister of Technology
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 MINI OF TECHNOLOGY, Minister of Technology filed Critical MINI OF TECHNOLOGY
Priority to GB36558/57A priority Critical patent/GB1120391A/en
Priority to US775656A priority patent/US3401634A/en
Publication of GB1120391A publication Critical patent/GB1120391A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/12—Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
    • 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
    • F02K9/28—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants having two or more propellant charges with the propulsion gases exhausting through a common nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

1,120,391. Self-propelled missiles. MINISTER OF TECHNOLOGY. 17 Nov., 1958 [22 Nov., 1957], No. 36558/57. Heading F3A. In a rocket having solid sustaining and booster charges, the latter are mounted at the rear of the sustaining charge which is ignited first. The hot gases from the sustaining charge pass along a cylindrical hole in the booster to the nozzle and ignite the booster which burns outwardly from the cylindrical hole and discharges through the same nozzle. As shown, the igniter 29 is fired by the wiring 36 and fires the sustainer charge 26, the hot gases from which pass through the nozzle 15, the tubular booster charge 32 and rearwardly through nozzle 19. The booster charge is ignited and the hot gases therein formed also flow through nozzle 19.
GB36558/57A 1957-11-22 1957-11-22 Improvements in or relating to rocketwise propelled projectiles Expired GB1120391A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB36558/57A GB1120391A (en) 1957-11-22 1957-11-22 Improvements in or relating to rocketwise propelled projectiles
US775656A US3401634A (en) 1957-11-22 1958-11-21 Rocketwise propelled projectiles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB36558/57A GB1120391A (en) 1957-11-22 1957-11-22 Improvements in or relating to rocketwise propelled projectiles

Publications (1)

Publication Number Publication Date
GB1120391A true GB1120391A (en) 1968-07-17

Family

ID=10389237

Family Applications (1)

Application Number Title Priority Date Filing Date
GB36558/57A Expired GB1120391A (en) 1957-11-22 1957-11-22 Improvements in or relating to rocketwise propelled projectiles

Country Status (2)

Country Link
US (1) US3401634A (en)
GB (1) GB1120391A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1985001320A1 (en) * 1983-09-16 1985-03-28 The Secretary Of State For Defence In Her Britanni Rocket with different charges
GB2314612B (en) * 1996-06-28 2000-12-13 Buck Chem Tech Werke A missile for combating moving targets
DE102014115722B4 (en) 2014-10-29 2022-08-11 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Integrated missile propulsion system

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3699891A (en) * 1969-04-23 1972-10-24 Susquehanna Corp Rocket vehicle and method of manufacturing same
US3807275A (en) * 1972-10-06 1974-04-30 Us Army Miniature missile system
US3855932A (en) * 1973-10-23 1974-12-24 Us Navy Expelling charge ignition system
US5596166A (en) * 1994-12-28 1997-01-21 Logicon Rda Penetrating vehicle with rocket motor

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB139856A (en) * 1919-02-03 1920-03-18 Garnett Senior Improvements in and connected with rockets
FR1058495A (en) * 1952-06-18 1954-03-16 Soc Tech De Rech Ind Jet thruster
FR1143581A (en) * 1954-05-14 1957-10-02 Soc Tech De Rech Ind Powder thruster

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1985001320A1 (en) * 1983-09-16 1985-03-28 The Secretary Of State For Defence In Her Britanni Rocket with different charges
EP0142246A1 (en) * 1983-09-16 1985-05-22 Royal Ordnance plc Rocket motor with two different charges
GB2314612B (en) * 1996-06-28 2000-12-13 Buck Chem Tech Werke A missile for combating moving targets
DE102014115722B4 (en) 2014-10-29 2022-08-11 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Integrated missile propulsion system

Also Published As

Publication number Publication date
US3401634A (en) 1968-09-17

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