BE836373A - Cloison pour propulseur de fusee - Google Patents
Cloison pour propulseur de fuseeInfo
- 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
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)
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 (fr) |
BE (1) | BE836373A (fr) |
DE (1) | DE2458180A1 (fr) |
FR (1) | FR2294334A1 (fr) |
GB (2) | GB1532988A (fr) |
IT (1) | IT1052526B (fr) |
SE (1) | SE7513787L (fr) |
Families Citing this family (19)
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 |
US4765134A (en) * | 1986-08-28 | 1988-08-23 | United Technologies Corporation | Acoustic oscillatory pressure control for solid propellant rocket |
ATE77474T1 (de) * | 1988-02-12 | 1992-07-15 | Fike Corp | Trennwandscheibe mit sollbruchstellen fuer raketen mit festen treibstoffen. |
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 |
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 |
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 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3127148A (en) * | 1964-03-31 | Valved coupling | ||
CA674719A (en) * | 1963-11-26 | S. Coffman Robert | Safety pressure relief device | |
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 |
-
1974
- 1974-12-09 DE DE19742458180 patent/DE2458180A1/de not_active Ceased
-
1975
- 1975-10-02 FR FR7530198A patent/FR2294334A1/fr not_active Withdrawn
- 1975-11-14 GB GB30269/78A patent/GB1532988A/en not_active Expired
- 1975-11-14 GB GB44752/75A patent/GB1532987A/en not_active Expired
- 1975-12-05 IT IT52561/75A patent/IT1052526B/it active
- 1975-12-05 US US05/637,958 patent/US4075832A/en not_active Expired - Lifetime
- 1975-12-08 BE BE162522A patent/BE836373A/fr unknown
- 1975-12-08 SE SE7513787A patent/SE7513787L/xx unknown
Also Published As
Publication number | Publication date |
---|---|
FR2294334A1 (fr) | 1976-07-09 |
DE2458180A1 (de) | 1976-06-10 |
IT1052526B (it) | 1981-07-20 |
GB1532987A (en) | 1978-11-22 |
SE7513787L (sv) | 1976-06-10 |
GB1532988A (en) | 1978-11-22 |
US4075832A (en) | 1978-02-28 |
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