AU8755398A - Case assembly including adhesive bond that is insensitive to high operating pressures and exhibits inherent high temperature relief capability, and mot or assembly and rocket assembly including the same - Google Patents

Case assembly including adhesive bond that is insensitive to high operating pressures and exhibits inherent high temperature relief capability, and mot or assembly and rocket assembly including the same

Info

Publication number
AU8755398A
AU8755398A AU87553/98A AU8755398A AU8755398A AU 8755398 A AU8755398 A AU 8755398A AU 87553/98 A AU87553/98 A AU 87553/98A AU 8755398 A AU8755398 A AU 8755398A AU 8755398 A AU8755398 A AU 8755398A
Authority
AU
Australia
Prior art keywords
assembly including
mot
insensitive
assembly
adhesive bond
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.)
Withdrawn
Application number
AU87553/98A
Inventor
Russell A. Crook
Joseph J. Kliger
Roger D. Wright
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of AU8755398A publication Critical patent/AU8755398A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/343—Joints, connections, seals therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
AU87553/98A 1997-02-28 1998-02-27 Case assembly including adhesive bond that is insensitive to high operating pressures and exhibits inherent high temperature relief capability, and mot or assembly and rocket assembly including the same Withdrawn AU8755398A (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US3957097P 1997-02-28 1997-02-28
US60039570 1997-02-28
US3984297P 1997-03-04 1997-03-04
US60039842 1997-03-04
PCT/US1998/003703 WO1998046960A2 (en) 1997-02-28 1998-02-27 Adhesive bonded case assembly for rockets

Publications (1)

Publication Number Publication Date
AU8755398A true AU8755398A (en) 1998-11-11

Family

ID=26716268

Family Applications (1)

Application Number Title Priority Date Filing Date
AU87553/98A Withdrawn AU8755398A (en) 1997-02-28 1998-02-27 Case assembly including adhesive bond that is insensitive to high operating pressures and exhibits inherent high temperature relief capability, and mot or assembly and rocket assembly including the same

Country Status (2)

Country Link
AU (1) AU8755398A (en)
WO (1) WO1998046960A2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010007404A1 (en) * 2010-02-09 2011-08-11 INPRO Innovationsgesellschaft für fortgeschrittene Produktionssysteme in der Fahrzeugindustrie mbH, 10587 Method for producing a tubular rotationally symmetrical motor vehicle chassis component such as a piston rod, and built piston rod
FR3011902B1 (en) * 2013-10-16 2015-11-27 Herakles METHOD FOR CONNECTING A JUPETTE TO AN ENVELOPE OF A PROPELLER BODY
CN107781062B (en) * 2017-09-28 2019-06-07 北京理工大学 A kind of Double pulse solid rocket motor interstage sealing structure device
CN114199092B (en) * 2021-12-13 2023-10-17 北京中科宇航技术有限公司 Rocket initiating explosive device ignition experimental container and design method thereof

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1203230A (en) * 1966-12-01 1970-08-26 Imp Metal Ind Kynoch Ltd Improvements in pressure vessels
DE2044170A1 (en) * 1970-09-05 1972-03-16 Bizien J Closure device for a pressurized chamber
US3784235A (en) * 1971-10-08 1974-01-08 Us Navy Tubular adhesive joint with snap lock
DE2855570C2 (en) * 1978-12-22 1985-06-20 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Rod-shaped component
US4602480A (en) * 1982-09-29 1986-07-29 Hercules Incorporated Threaded polar openings for composite pressure vessels
FR2593238B1 (en) * 1986-01-22 1990-11-02 Europ Propulsion PROPELLER COMBUSTION CHAMBER AND ASSEMBLY METHOD
US5394803A (en) * 1994-02-14 1995-03-07 Bel Electronics, Inc. Joint construction between military rocket motor and warhead and releasable by melting of fusible eutectic wedging ring for operating flexible locking fingers
US5613794A (en) * 1994-08-16 1997-03-25 Hong Kong (Link) Bicycles Ltd. Bi-material tubing and method of making same

Also Published As

Publication number Publication date
WO1998046960A2 (en) 1998-10-22
WO1998046960A3 (en) 1999-02-18

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