GB590177A - Improvements in or relating to projectiles of the rocket type - Google Patents

Improvements in or relating to projectiles of the rocket type

Info

Publication number
GB590177A
GB590177A GB1360644A GB1360644A GB590177A GB 590177 A GB590177 A GB 590177A GB 1360644 A GB1360644 A GB 1360644A GB 1360644 A GB1360644 A GB 1360644A GB 590177 A GB590177 A GB 590177A
Authority
GB
United Kingdom
Prior art keywords
cordite
fuel
valve
combustion
projectile
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
GB1360644A
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.)
HYDRAN PRODUCTS Ltd
Original Assignee
HYDRAN PRODUCTS Ltd
Filing date
Publication date
Application filed by HYDRAN PRODUCTS Ltd filed Critical HYDRAN PRODUCTS Ltd
Publication of GB590177A publication Critical patent/GB590177A/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
    • 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
    • F02K7/105—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 using a solid fuel
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

590,177. Projectiles. HYDRAN PRODUCTS, Ltd., and MOTLEY, L. July 17, 1944, No. 13606. [Classes 9 (i) and 9 (ii)] A rocket projectile is launched and initially propelled by a combustible such as cordite which contains its own oxygen and is carried by the projectile and subsequently by the combustion of fuel with the ambient air. The cordite is contained in chamber 1 and the products of combustion are discharged through orifices 2. The liquid fuel is contained in a surrounding chamber 3 and is heated by the combustion of the cordite. A valve 9 allows the fuel to pass to the main chamber 1 by a narow gauge passage 8 when the pressure in this chamber falls due to burning out of the cordite charge. Similarly a valve 7 allows air to enter when the air pressure due to the velocity of the projectile is greater than that of the burning cordite charge. The pressure generated by combustion, of the fuel and air recloses the valve and the cycle is repeated until the fuel is exhausted. The valve 7 comprises a cone having radial slots 7b closed by flap valve members 7c. The orifices 2 are arranged to stabilize the projectile by rotation. The nose 4 may contain an explosive charge. Reference has been directed by the Comptroller to Specification 579,807.
GB1360644A 1944-07-17 Improvements in or relating to projectiles of the rocket type Expired GB590177A (en)

Publications (1)

Publication Number Publication Date
GB590177A true GB590177A (en) 1947-07-10

Family

ID=1729360

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1360644A Expired GB590177A (en) 1944-07-17 Improvements in or relating to projectiles of the rocket type

Country Status (1)

Country Link
GB (1) GB590177A (en)

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2631425A (en) * 1948-09-11 1953-03-17 Bofors Ab Compression nozzle for ram-jet engines
US2637161A (en) * 1949-11-10 1953-05-05 Us Army Process of ignition for rockets and the like
US2677232A (en) * 1948-06-05 1954-05-04 Continental Aviat & Engineerin Combination pulse jet and ram jet engine
US2684570A (en) * 1949-06-16 1954-07-27 Bofors Ab Rocket-engine and reaction-motor missile
US2711630A (en) * 1951-12-28 1955-06-28 Lehman Sylvester Clyde Rockets
US2743575A (en) * 1951-03-24 1956-05-01 Witold B Brzozowski Valveless intermittent combustor with automatic flow control
US2745248A (en) * 1950-10-12 1956-05-15 Mcdonnell Aircraft Corp Convertible pulse jet and ram jet engine
US2807209A (en) * 1952-05-20 1957-09-24 Jarman G Kennard Fuel pressurization system
US2883829A (en) * 1955-01-24 1959-04-28 Curtiss Wright Corp Rocket engine convertible to a ramjet engine
US2912820A (en) * 1953-07-31 1959-11-17 Quentin R Whitmore Combined ram jet and rocket engine
US2918004A (en) * 1952-10-21 1959-12-22 Denovan Alexander Ewi Crawford Electrically heated jet propulsion unit
US2938482A (en) * 1956-05-31 1960-05-31 Floyd A Newburn Solid propellant starter for liquid fuel monopropellant torpedo propulsion system
US2948112A (en) * 1953-12-14 1960-08-09 Kenneth W Smith Combined rocket and ram-jet engine
US2998703A (en) * 1953-09-11 1961-09-05 William C Badders Reso-jet igniter
US3024729A (en) * 1948-04-24 1962-03-13 Cornell Aeronautical Labor Inc Ram jet projectile
US3182445A (en) * 1959-12-21 1965-05-11 Dow Chemical Co Liquid-solid propellant rocket case and method
US3724216A (en) * 1957-06-13 1973-04-03 Us Navy Combined rocket-ram-jet aircraft
US3768255A (en) * 1967-03-06 1973-10-30 Texaco Inc Inlet port covers for reaction vehicle
US4050243A (en) * 1976-05-17 1977-09-27 The United States Of America As Represented By The Secretary Of The Navy Combination solid fuel ramjet injector/port cover
US4381642A (en) * 1980-06-20 1983-05-03 The Boeing Company Ramjet engine
US4651523A (en) * 1984-10-06 1987-03-24 Rolls-Royce Plc Integral rocket and ramjet engine
US8079308B1 (en) * 1988-10-12 2011-12-20 Aerospatiale Societe Nationale Industrielle Ramjet engine incorporating a tubular structure and a missile propelled by a ramjet engines of this type
RU2760039C1 (en) * 2021-07-12 2021-11-22 Владислав Юрьевич Климов Cruise missile
CN115107968A (en) * 2022-06-13 2022-09-27 南昌航空大学 Low-navigation-speed underwater ramjet engine and design method thereof

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3024729A (en) * 1948-04-24 1962-03-13 Cornell Aeronautical Labor Inc Ram jet projectile
US2677232A (en) * 1948-06-05 1954-05-04 Continental Aviat & Engineerin Combination pulse jet and ram jet engine
US2631425A (en) * 1948-09-11 1953-03-17 Bofors Ab Compression nozzle for ram-jet engines
US2684570A (en) * 1949-06-16 1954-07-27 Bofors Ab Rocket-engine and reaction-motor missile
US2637161A (en) * 1949-11-10 1953-05-05 Us Army Process of ignition for rockets and the like
US2745248A (en) * 1950-10-12 1956-05-15 Mcdonnell Aircraft Corp Convertible pulse jet and ram jet engine
US2743575A (en) * 1951-03-24 1956-05-01 Witold B Brzozowski Valveless intermittent combustor with automatic flow control
US2711630A (en) * 1951-12-28 1955-06-28 Lehman Sylvester Clyde Rockets
US2807209A (en) * 1952-05-20 1957-09-24 Jarman G Kennard Fuel pressurization system
US2918004A (en) * 1952-10-21 1959-12-22 Denovan Alexander Ewi Crawford Electrically heated jet propulsion unit
US2912820A (en) * 1953-07-31 1959-11-17 Quentin R Whitmore Combined ram jet and rocket engine
US2998703A (en) * 1953-09-11 1961-09-05 William C Badders Reso-jet igniter
US2948112A (en) * 1953-12-14 1960-08-09 Kenneth W Smith Combined rocket and ram-jet engine
US2883829A (en) * 1955-01-24 1959-04-28 Curtiss Wright Corp Rocket engine convertible to a ramjet engine
US2938482A (en) * 1956-05-31 1960-05-31 Floyd A Newburn Solid propellant starter for liquid fuel monopropellant torpedo propulsion system
US3724216A (en) * 1957-06-13 1973-04-03 Us Navy Combined rocket-ram-jet aircraft
US3182445A (en) * 1959-12-21 1965-05-11 Dow Chemical Co Liquid-solid propellant rocket case and method
US3768255A (en) * 1967-03-06 1973-10-30 Texaco Inc Inlet port covers for reaction vehicle
US4050243A (en) * 1976-05-17 1977-09-27 The United States Of America As Represented By The Secretary Of The Navy Combination solid fuel ramjet injector/port cover
US4381642A (en) * 1980-06-20 1983-05-03 The Boeing Company Ramjet engine
US4651523A (en) * 1984-10-06 1987-03-24 Rolls-Royce Plc Integral rocket and ramjet engine
US8079308B1 (en) * 1988-10-12 2011-12-20 Aerospatiale Societe Nationale Industrielle Ramjet engine incorporating a tubular structure and a missile propelled by a ramjet engines of this type
RU2760039C1 (en) * 2021-07-12 2021-11-22 Владислав Юрьевич Климов Cruise missile
CN115107968A (en) * 2022-06-13 2022-09-27 南昌航空大学 Low-navigation-speed underwater ramjet engine and design method thereof
CN115107968B (en) * 2022-06-13 2023-04-18 南昌航空大学 Low-navigational-speed underwater ramjet engine and design method thereof

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