BE836373A - Cloison pour propulseur de fusee - Google Patents

Cloison pour propulseur de fusee

Info

Publication number
BE836373A
BE836373A BE162522A BE162522A BE836373A BE 836373 A BE836373 A BE 836373A BE 162522 A BE162522 A BE 162522A BE 162522 A BE162522 A BE 162522A BE 836373 A BE836373 A BE 836373A
Authority
BE
Belgium
Prior art keywords
bulkhead
rocket thruster
thruster
rocket
Prior art date
Application number
BE162522A
Other languages
English (en)
French (fr)
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 filed Critical
Publication of BE836373A publication Critical patent/BE836373A/xx

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
    • F02K9/28—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
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/1624—Destructible or deformable element controlled
    • Y10T137/1632—Destructible element
    • Y10T137/1782—Frangible element returns pressure responsive valve
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7837—Direct response valves [i.e., check valve type]
    • Y10T137/7869—Biased open
    • Y10T137/7875—Pivoted valves
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7837—Direct response valves [i.e., check valve type]
    • Y10T137/7898—Pivoted valves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
BE162522A 1974-12-09 1975-12-08 Cloison pour propulseur de fusee BE836373A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19742458180 DE2458180A1 (de) 1974-12-09 1974-12-09 Trennwand fuer raketentriebwerke

Publications (1)

Publication Number Publication Date
BE836373A true BE836373A (fr) 1976-04-01

Family

ID=5932947

Family Applications (1)

Application Number Title Priority Date Filing Date
BE162522A BE836373A (fr) 1974-12-09 1975-12-08 Cloison pour propulseur de fusee

Country Status (7)

Country Link
US (1) US4075832A (sv)
BE (1) BE836373A (sv)
DE (1) DE2458180A1 (sv)
FR (1) FR2294334A1 (sv)
GB (2) GB1532988A (sv)
IT (1) IT1052526B (sv)
SE (1) SE7513787L (sv)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1537469A (en) * 1975-12-23 1978-12-29 Imi Kynoch Ltd Disintegrable member for controlling flow between pressure chambers
US4230150A (en) * 1979-02-22 1980-10-28 Domer Scaramucci Tilting disc check valve
DE3005864A1 (de) * 1980-02-16 1981-09-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum steuern der stroemungsquerschnitte von kanaelen, insbesondere von gasleitrohren eines raketen-staustrahltriebwerks
DE3115187C2 (de) * 1981-04-15 1983-04-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "Ventil mit drehbar angeordnetem Ventilkörper, insbesondere zum Dosieren der brennstoffreichen Gase von Staustrahl-Raketentriebwerken"
US4864817A (en) * 1983-05-26 1989-09-12 Morton Thiokol, Inc. Membrane seal for application to pulsed rocket motor
US4840024A (en) * 1984-08-20 1989-06-20 Morton Thiokol, Inc. Multiple propellant solid rocket motor
GB2165338B (en) * 1984-10-06 1988-11-02 Rolls Royce Integral rocket and ramjet engine
US4605041A (en) * 1985-04-05 1986-08-12 Teumer Henry E Check valve
FR2584456B1 (fr) * 1985-07-03 1987-10-02 Poudres & Explosifs Ste Nale Dispositif de fermeture temporaire d'un orifice interne d'un propulseur
US4829765A (en) * 1985-12-27 1989-05-16 Morton Thiokol, Inc. Pulsed rocket motor
EP0327662B1 (en) * 1988-02-12 1992-06-17 Fike Corporation Bulkhead rupture disc for solid propellant missiles
US4765134A (en) * 1986-08-28 1988-08-23 United Technologies Corporation Acoustic oscillatory pressure control for solid propellant rocket
US5160070A (en) * 1988-08-11 1992-11-03 Fike Corporation Reverse bulged forward acting scored rupture disc bulkhead structure for multi-stage rocket motor
GB9206616D0 (en) * 1992-03-26 1997-09-17 Royal Ordnance Plc Improvements in or relating to combustion apparatus and valves therefor
US5419118A (en) * 1994-01-19 1995-05-30 Universal Propulsion Company, Inc. Multi-stage rocket motors
US5579636A (en) * 1995-03-21 1996-12-03 Aerotech, Inc. Pyrotechnic valve, igniter and combustion preheater for hybrid rocket motors
US7814835B2 (en) * 2008-02-26 2010-10-19 Zhongwei Shi Propulsion enhancement arrangement for rocket
CN110594039A (zh) * 2019-08-20 2019-12-20 西安航天动力技术研究所 一种降低双脉冲固体发动机隔层应变的隔层结构
CN110566367B (zh) * 2019-08-20 2021-09-03 西安航天动力技术研究所 一种降低双脉冲固体发动机隔层应变的燃烧室

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA674719A (en) * 1963-11-26 S. Coffman Robert Safety pressure relief device
US3127148A (en) * 1964-03-31 Valved coupling
US2358101A (en) * 1943-03-23 1944-09-12 Merwyn C Randall Relief valve
US2553267A (en) * 1946-10-09 1951-05-15 Andrew R Nedoh Shear diaphragm relief union
US2831499A (en) * 1954-09-07 1958-04-22 Rohr Aircraft Corp Check valve
US2923317A (en) * 1955-11-17 1960-02-02 Crane Co Swing check valve
US2905358A (en) * 1957-04-29 1959-09-22 Allis Chalmers Mfg Co Relief valve
US3039482A (en) * 1961-01-17 1962-06-19 Thiokol Chemical Corp Offset hermetic seal for butterfly type valve
GB1012023A (en) * 1961-06-14 1965-12-08 Bristol Aerojet Ltd Improvements in rocket motors
US3191619A (en) * 1962-09-18 1965-06-29 Cameron Iron Works Inc Check valve having movably mounted head and seat
US3691770A (en) * 1966-12-02 1972-09-19 Us Navy Thrust control means for a solid propellant rocket motor
US3640306A (en) * 1970-10-19 1972-02-08 Bobrick Aero Missile Products Pressure relief valve
DE2214802A1 (de) * 1972-03-25 1973-09-27 Dynamit Nobel Ag Feststoffraketenmotor
DE2230457C3 (de) * 1972-06-22 1981-05-27 Dynamit Nobel Ag, 5210 Troisdorf Zwischenwand für Raketentriebwerke
US3831628A (en) * 1973-03-13 1974-08-27 E Kintner Check valve

Also Published As

Publication number Publication date
SE7513787L (sv) 1976-06-10
DE2458180A1 (de) 1976-06-10
IT1052526B (it) 1981-07-20
FR2294334A1 (fr) 1976-07-09
GB1532988A (en) 1978-11-22
GB1532987A (en) 1978-11-22
US4075832A (en) 1978-02-28

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