DE60142312D1 - Raketenmotor mit temperaturabhängigem sicherheitsmechanismus - Google Patents

Raketenmotor mit temperaturabhängigem sicherheitsmechanismus

Info

Publication number
DE60142312D1
DE60142312D1 DE60142312T DE60142312T DE60142312D1 DE 60142312 D1 DE60142312 D1 DE 60142312D1 DE 60142312 T DE60142312 T DE 60142312T DE 60142312 T DE60142312 T DE 60142312T DE 60142312 D1 DE60142312 D1 DE 60142312D1
Authority
DE
Germany
Prior art keywords
safety mechanism
temperature dependent
rocket motor
dependent safety
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.)
Expired - Lifetime
Application number
DE60142312T
Other languages
German (de)
English (en)
Inventor
Mark A Solberg
Robert E Black
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.)
Northrop Grumman Innovation Systems LLC
Original Assignee
Alliant Techsystems Inc
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 Alliant Techsystems Inc filed Critical Alliant Techsystems Inc
Application granted granted Critical
Publication of DE60142312D1 publication Critical patent/DE60142312D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
    • F42B39/20—Packages or ammunition having valves for pressure-equalising; Packages or ammunition having plugs for pressure release, e.g. meltable ; Blow-out panels; Venting arrangements
    • 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
    • F02K9/38—Safety devices, e.g. to prevent accidental ignition

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Testing Of Engines (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Portable Nailing Machines And Staplers (AREA)
DE60142312T 2001-11-01 2001-11-01 Raketenmotor mit temperaturabhängigem sicherheitsmechanismus Expired - Lifetime DE60142312D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2001/048170 WO2003046359A1 (en) 2001-11-01 2001-11-01 Rocket motors with insensitive munitions systems

Publications (1)

Publication Number Publication Date
DE60142312D1 true DE60142312D1 (de) 2010-07-15

Family

ID=21743116

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60142312T Expired - Lifetime DE60142312D1 (de) 2001-11-01 2001-11-01 Raketenmotor mit temperaturabhängigem sicherheitsmechanismus

Country Status (7)

Country Link
EP (1) EP1440233B1 (enExample)
JP (1) JP4091916B2 (enExample)
AU (1) AU2001297861B2 (enExample)
CA (1) CA2465295C (enExample)
DE (1) DE60142312D1 (enExample)
IL (2) IL161612A0 (enExample)
WO (1) WO2003046359A1 (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6883817B2 (ja) * 2017-02-10 2021-06-09 株式会社Ｉｈｉエアロスペース ロケットモータ
CN107044914A (zh) * 2017-03-16 2017-08-15 中国人民解放军海军航空工程学院 固体发动机粘接界面受载状态监检测装置
IL260886B (en) * 2018-07-30 2021-04-29 Rafael Advanced Defense Systems Ltd Rocket armament that can be launched from a tubular launcher with non-ignition security outside the launcher and engine separation in flight

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4597261A (en) * 1984-05-25 1986-07-01 Hughes Aircraft Company Thermally actuated rocket motor safety system
US5129326A (en) * 1987-04-14 1992-07-14 Aerojet-General Corporation Ordnance device with explosion protection
US5786544A (en) * 1994-03-02 1998-07-28 State of Israel--Ministry of Defence, Armament Development Authority, Rafael Warhead protection device during slow cook-off test
US5813219A (en) * 1994-03-02 1998-09-29 State Of Israel - Ministry Of Defence Armament Development Authority, Rafael Rocket motor protection device during slow cook-off test
US5792981A (en) * 1996-10-28 1998-08-11 Thiokol Corporation Gun-launched rocket

Also Published As

Publication number Publication date
AU2001297861A1 (en) 2003-06-10
EP1440233B1 (en) 2010-06-02
AU2001297861B2 (en) 2008-05-01
CA2465295A1 (en) 2003-06-05
JP2005510653A (ja) 2005-04-21
WO2003046359A1 (en) 2003-06-05
JP4091916B2 (ja) 2008-05-28
CA2465295C (en) 2009-09-22
IL161612A (en) 2006-12-31
IL161612A0 (en) 2004-09-27
EP1440233A1 (en) 2004-07-28

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