AU4734779A - Two-way rocket plenum for combustion suppression - Google Patents

Two-way rocket plenum for combustion suppression

Info

Publication number
AU4734779A
AU4734779A AU47347/79A AU4734779A AU4734779A AU 4734779 A AU4734779 A AU 4734779A AU 47347/79 A AU47347/79 A AU 47347/79A AU 4734779 A AU4734779 A AU 4734779A AU 4734779 A AU4734779 A AU 4734779A
Authority
AU
Australia
Prior art keywords
plenum
combustion suppression
rocket
way
way 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.)
Granted
Application number
AU47347/79A
Other versions
AU518428B2 (en
Inventor
Edward T. Piesik
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.)
Hughes Missile Systems Co
Original Assignee
General Dynamics Corp
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
Priority to GB7917780A priority Critical patent/GB2051320B/en
Application filed by General Dynamics Corp filed Critical General Dynamics Corp
Priority to AU47347/79A priority patent/AU518428B2/en
Priority to NL7904296A priority patent/NL7904296A/en
Priority to FR7914617A priority patent/FR2458678A1/en
Priority to DE19792923755 priority patent/DE2923755A1/en
Priority to CH558679A priority patent/CH629889A5/en
Publication of AU4734779A publication Critical patent/AU4734779A/en
Application granted granted Critical
Publication of AU518428B2 publication Critical patent/AU518428B2/en
Assigned to HUGHES MISSILE SYSTEMS COMPANY reassignment HUGHES MISSILE SYSTEMS COMPANY Alteration of Name(s) in Register under S187 Assignors: GENERAL DYNAMICS CORPORATION
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
    • F15D1/00—Influencing flow of fluids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/0413—Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/073—Silos for rockets, e.g. mounting or sealing rockets therein

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Exhaust Silencers (AREA)
  • Testing Of Engines (AREA)
AU47347/79A 1979-05-22 1979-05-23 Two-way rocket plenum for combustion suppression Ceased AU518428B2 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB7917780A GB2051320B (en) 1979-05-22 1979-05-22 Two-way rocket plenum for combustion suppression
AU47347/79A AU518428B2 (en) 1979-05-22 1979-05-23 Two-way rocket plenum for combustion suppression
NL7904296A NL7904296A (en) 1979-05-22 1979-05-31 COLLECTION CHAMBER FOR ROCKET COMBUSTION GASES.
FR7914617A FR2458678A1 (en) 1979-05-22 1979-06-07 TWO-WAY EXHAUST GAS MANIFOLD, IN PARTICULAR FOR FLARE LAUNCHERS
DE19792923755 DE2923755A1 (en) 1979-05-22 1979-06-12 2-WAY COLLECTING CHAMBER FOR ROCKET EXHAUST GAS TO SUPPRESS COMBUSTION
CH558679A CH629889A5 (en) 1979-05-22 1979-06-14 ROCKET EXHAUST GAS COLLECTOR.

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
GB7917780A GB2051320B (en) 1979-05-22 1979-05-22 Two-way rocket plenum for combustion suppression
AU47347/79A AU518428B2 (en) 1979-05-22 1979-05-23 Two-way rocket plenum for combustion suppression
NL7904296A NL7904296A (en) 1979-05-22 1979-05-31 COLLECTION CHAMBER FOR ROCKET COMBUSTION GASES.
FR7914617A FR2458678A1 (en) 1979-05-22 1979-06-07 TWO-WAY EXHAUST GAS MANIFOLD, IN PARTICULAR FOR FLARE LAUNCHERS
DE19792923755 DE2923755A1 (en) 1979-05-22 1979-06-12 2-WAY COLLECTING CHAMBER FOR ROCKET EXHAUST GAS TO SUPPRESS COMBUSTION
CH558679A CH629889A5 (en) 1979-05-22 1979-06-14 ROCKET EXHAUST GAS COLLECTOR.

Publications (2)

Publication Number Publication Date
AU4734779A true AU4734779A (en) 1980-11-27
AU518428B2 AU518428B2 (en) 1981-10-01

Family

ID=27542722

Family Applications (1)

Application Number Title Priority Date Filing Date
AU47347/79A Ceased AU518428B2 (en) 1979-05-22 1979-05-23 Two-way rocket plenum for combustion suppression

Country Status (6)

Country Link
AU (1) AU518428B2 (en)
CH (1) CH629889A5 (en)
DE (1) DE2923755A1 (en)
FR (1) FR2458678A1 (en)
GB (1) GB2051320B (en)
NL (1) NL7904296A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2124741B (en) * 1982-07-15 1986-01-08 British Aerospace Missile launcher
GB2290856B (en) * 1983-09-07 1996-06-26 Royal Ordnance Plc Missile storage apparatus
GB8323984D0 (en) * 1983-09-07 1995-04-05 Imi Kynoch Ltd Missile storage apparatus
US6584882B2 (en) * 2001-01-22 2003-07-01 Lockheed Martin Corporation Self-contained canister missile launcher with tubular exhaust uptake ducts
CN115127394B (en) * 2022-06-08 2023-07-28 中国人民解放军96901部队22分队 Rocket ejection power gas pressure equalizing, pressure reducing and rectifying device and control method

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2925013A (en) * 1956-05-01 1960-02-16 North American Aviation Inc Rocket engine assembly testing and launching apparatus
US2987964A (en) * 1957-12-02 1961-06-13 American Mach & Foundry Missile launcher
US3011406A (en) * 1959-07-28 1961-12-05 Otto P Werle Missile launching system
NL262078A (en) * 1960-03-11
US3228296A (en) * 1963-05-23 1966-01-11 Milton C Neuman Arrangement for venting blast gases and for water injection
US3363508A (en) * 1965-04-19 1968-01-16 Stahmer Bernhardt Rocket launcher
US4044648A (en) * 1975-09-29 1977-08-30 General Dynamics Corporation Rocket exhaust plenum flow control apparatus
US4134327A (en) * 1977-12-12 1979-01-16 General Dynamics Corporation Rocket launcher tube post-launch rear closure

Also Published As

Publication number Publication date
FR2458678A1 (en) 1981-01-02
NL7904296A (en) 1980-12-02
DE2923755A1 (en) 1981-01-15
GB2051320B (en) 1983-09-28
GB2051320A (en) 1981-01-14
AU518428B2 (en) 1981-10-01
FR2458678B1 (en) 1984-06-29
CH629889A5 (en) 1982-05-14

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