SE439685B - Anordning for avfyrning av ett flertal reaktionsdrivna farkoster - Google Patents

Anordning for avfyrning av ett flertal reaktionsdrivna farkoster

Info

Publication number
SE439685B
SE439685B SE7905675A SE7905675A SE439685B SE 439685 B SE439685 B SE 439685B SE 7905675 A SE7905675 A SE 7905675A SE 7905675 A SE7905675 A SE 7905675A SE 439685 B SE439685 B SE 439685B
Authority
SE
Sweden
Prior art keywords
exhaust
firing tube
portions
lid
firing
Prior art date
Application number
SE7905675A
Other languages
English (en)
Swedish (sv)
Other versions
SE7905675L (sv
Inventor
E T Piesik
Original Assignee
Gen 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
Application filed by Gen Dynamics Corp filed Critical Gen Dynamics Corp
Publication of SE7905675L publication Critical patent/SE7905675L/
Publication of SE439685B publication Critical patent/SE439685B/sv

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/0413Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/077Doors or covers for launching tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Exhaust Silencers (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Sealing Devices (AREA)
  • Refuse Collection And Transfer (AREA)
  • Testing Of Engines (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Processing Of Solid Wastes (AREA)
  • Pipe Accessories (AREA)
SE7905675A 1978-08-09 1979-06-28 Anordning for avfyrning av ett flertal reaktionsdrivna farkoster SE439685B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/932,245 US4186647A (en) 1978-08-09 1978-08-09 Multiple area rear launch tube cover

Publications (2)

Publication Number Publication Date
SE7905675L SE7905675L (sv) 1980-02-10
SE439685B true SE439685B (sv) 1985-06-24

Family

ID=25462015

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7905675A SE439685B (sv) 1978-08-09 1979-06-28 Anordning for avfyrning av ett flertal reaktionsdrivna farkoster

Country Status (15)

Country Link
US (1) US4186647A (fr)
JP (1) JPS5914720B2 (fr)
AU (1) AU512640B2 (fr)
BE (1) BE877898A (fr)
CA (1) CA1105721A (fr)
CH (1) CH635670A5 (fr)
DE (1) DE2931618C2 (fr)
DK (1) DK150256C (fr)
ES (1) ES483020A1 (fr)
FR (1) FR2433168A1 (fr)
GB (1) GB2027519B (fr)
IT (1) IT1117442B (fr)
NL (1) NL180354B (fr)
NO (1) NO146883C (fr)
SE (1) SE439685B (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4324167A (en) * 1980-04-14 1982-04-13 General Dynamics, Pomona Division Flexible area launch tube rear cover
US4373420A (en) * 1980-10-06 1983-02-15 General Dynamics, Pomona Division Combustion suppressor
JPS60186248U (ja) * 1984-05-23 1985-12-10 マツダ株式会社 自動車の二列目シ−ト装置
US4683798A (en) * 1985-12-27 1987-08-04 General Dynamics, Pomona Division Gas management transition device
US4686884A (en) * 1985-12-27 1987-08-18 General Dynamics, Pomona Division Gas management deflector
US4796510A (en) * 1987-11-09 1989-01-10 General Dynamics, Pomona Division Rocket exhaust recirculation obturator for missile launch tube
US4756226A (en) * 1987-11-09 1988-07-12 General Dynamics, Pomona Division Missile support structure for a launch tube
US4934241A (en) * 1987-11-12 1990-06-19 General Dynamics Corp. Pomona Division Rocket exhaust deflector
GB8825195D0 (en) * 1988-10-27 1989-04-19 British Aerospace Impingement pressure regulator
US5058481A (en) * 1990-10-15 1991-10-22 The United States Of America As Represented By The Secretary Of The Navy Dual modular rocket launcher
US5162605A (en) * 1992-01-16 1992-11-10 General Dynamics Corporation Self-activated rocket launcher cell closure
FR2711966B1 (fr) * 1993-11-04 1995-12-22 France Etat Armement Dispositif d'évacuation des gaz de combustion de missiles sur un navire.
US8584569B1 (en) * 2011-12-06 2013-11-19 The United States Of America As Represented By The Secretary Of The Navy Plume exhaust management for VLS
US9874420B2 (en) * 2013-12-30 2018-01-23 Bae Systems Land & Armaments, L.P. Missile canister gated obturator
CN116499309B (zh) * 2023-06-29 2023-11-24 北京坤飞航天科技有限公司 一种火箭发射台热防护结构及制作方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445423A (en) * 1946-03-06 1948-07-20 United Shoe Machinery Corp Safety container for rockets
US3499364A (en) * 1959-11-19 1970-03-10 Us Navy Apparatus for submerged launching of missiles
US3079752A (en) * 1961-02-23 1963-03-05 Thompson Ramo Wooldridge Inc Variable expansion ratio nozzle
US3228296A (en) * 1963-05-23 1966-01-11 Milton C Neuman Arrangement for venting blast gases and for water injection
US3198073A (en) * 1963-11-06 1965-08-03 Johns Manville Rupturable heat shield
US3237402A (en) * 1963-11-14 1966-03-01 Steverding Bernard Variable thrust nozzle
US3309874A (en) * 1965-02-04 1967-03-21 Bert B Gould Ablative nozzle
FR2127109A5 (fr) * 1971-02-24 1972-10-13 France Etat
US3897962A (en) * 1971-03-16 1975-08-05 Allied Chem Gas generator nozzle
US3893366A (en) * 1973-10-29 1975-07-08 Us Navy Missile launcher guide assembly
US3968646A (en) * 1974-06-28 1976-07-13 The United States Of America As Represented By The Secretary Of The Army Noise controllable nozzle closure
FR2296834A1 (fr) * 1974-12-31 1976-07-30 Poudres & Explosifs Ste Nale Dispositif pyrotechnique a double charge comportant une securite sequentielle
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
AU4927379A (en) 1980-03-20
GB2027519B (en) 1982-11-10
FR2433168B1 (fr) 1983-10-28
NO146883B (no) 1982-09-13
CH635670A5 (fr) 1983-04-15
FR2433168A1 (fr) 1980-03-07
DK150256B (da) 1987-01-19
DK332079A (da) 1980-02-10
BE877898A (fr) 1980-01-28
AU512640B2 (en) 1980-10-23
NO792580L (no) 1980-02-12
IT1117442B (it) 1986-02-17
DE2931618A1 (de) 1980-02-28
NL180354B (nl) 1986-09-01
NL7905378A (nl) 1980-02-12
DE2931618C2 (de) 1982-09-30
GB2027519A (en) 1980-02-20
US4186647A (en) 1980-02-05
ES483020A1 (es) 1980-08-16
NO146883C (no) 1982-12-22
DK150256C (da) 1987-10-12
SE7905675L (sv) 1980-02-10
CA1105721A (fr) 1981-07-28
IT7949979A0 (it) 1979-08-07
JPS5914720B2 (ja) 1984-04-05
JPS5525794A (en) 1980-02-23

Similar Documents

Publication Publication Date Title
SE439685B (sv) Anordning for avfyrning av ett flertal reaktionsdrivna farkoster
US4324167A (en) Flexible area launch tube rear cover
US3759039A (en) Thrust control and modulation system
US4993314A (en) Convectively cooled hot gas exhaust structure to reduce infrared radiation
JPS6314167B2 (fr)
US4173919A (en) Two-way rocket plenum for combustion suppression
US5194688A (en) Apparatus for limiting recirculation of rocket exhaust gases during missile launch
Webster Liquid fueled integral rocket/ramjet technology review
US20130014487A1 (en) Packaged propellant air-induced variable thrust rocket engine
US3196610A (en) Solid propellant rocket motor having reverse thrust generating means
US4683798A (en) Gas management transition device
KR101494393B1 (ko) 이중 추력 로켓 추진기관
CN108343765B (zh) 一种爆炸式阀门及其应用以及提升能量转化效率的方法
EP1801402A2 (fr) Tuyères de poussée à réglage fluidique avec combustion pulsée
US3313113A (en) Control for opening nozzles of rocket engines
US2787194A (en) Gun installation in jet aircraft
US3296799A (en) Thrust vector control system
EP0551991B1 (fr) Couvercle à action automatique pour une cellule d'un lanceur de missiles
US2708340A (en) Gas control in afterburner
CN208169627U (zh) 一种爆炸式阀门、叶轮动力装置和发动机
US3300142A (en) Rocket nozzle capable of inducing flow separation
US3034294A (en) Exhaust nozzle burning supersonic ramjet
US3134222A (en) Rocket engine control
US3112903A (en) Combination fuel tank and ram jet power plant
KR830001723Y1 (ko) 후미 발사관 커버

Legal Events

Date Code Title Description
NUG Patent has lapsed

Ref document number: 7905675-0

Effective date: 19940110

Format of ref document f/p: F