NL6817607A - - Google Patents

Info

Publication number
NL6817607A
NL6817607A NL6817607A NL6817607A NL6817607A NL 6817607 A NL6817607 A NL 6817607A NL 6817607 A NL6817607 A NL 6817607A NL 6817607 A NL6817607 A NL 6817607A NL 6817607 A NL6817607 A NL 6817607A
Authority
NL
Netherlands
Application number
NL6817607A
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 NL6817607A publication Critical patent/NL6817607A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/28Rocket-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10Shape or structure of solid propellant charges
    • F02K9/12Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Solid-Fuel Combustion (AREA)
NL6817607A 1968-01-16 1968-12-09 NL6817607A (xx)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19681626079 DE1626079A1 (de) 1968-01-16 1968-01-16 Dual-Festtreibstoff-Raketentriebwerk

Publications (1)

Publication Number Publication Date
NL6817607A true NL6817607A (xx) 1969-07-18

Family

ID=5682985

Family Applications (1)

Application Number Title Priority Date Filing Date
NL6817607A NL6817607A (xx) 1968-01-16 1968-12-09

Country Status (7)

Country Link
US (1) US3555825A (xx)
BE (1) BE726920A (xx)
DE (1) DE1626079A1 (xx)
FR (1) FR1600673A (xx)
GB (1) GB1216823A (xx)
NL (1) NL6817607A (xx)
SE (1) SE336933B (xx)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3665706A (en) * 1970-10-22 1972-05-30 Us Navy Igniter-attenuator device for attenuating combustion instability in rocket motors
US4655417A (en) * 1984-09-28 1987-04-07 The Boeing Company Molded ejection seat having an integrated rocket motor assembly
USRE49778E1 (en) 2007-03-22 2024-01-02 Firehawk Aerospace, Inc. Persistent vortex generating high regression rate solid fuel grain for a hybrid rocket engine
USRE49765E1 (en) 2007-03-22 2023-12-26 Firehawk Aerospace, Inc. Additive manufactured thermoplastic-nanocomposite aluminum hybrid rocket fuel grain and method of manufacturing same
US20100011742A1 (en) * 2008-07-17 2010-01-21 Cavalleri Robert J Rocket Motor Containing Multiple Pellet Cells
US8242422B2 (en) * 2009-02-23 2012-08-14 Raytheon Company Modular divert and attitude control system
US8667776B2 (en) 2009-02-23 2014-03-11 Raytheon Company Pellet-loaded multiple impulse rocket motor
US20110024165A1 (en) 2009-07-31 2011-02-03 Raytheon Company Systems and methods for composite structures with embedded interconnects
US8826640B2 (en) 2010-11-12 2014-09-09 Raytheon Company Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof
DE102011103221B4 (de) * 2011-06-01 2015-08-20 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Vorrichtung zur Schuberzeugung
JP6125370B2 (ja) 2013-08-13 2017-05-10 三菱重工業株式会社 マルチパルスガスジェネレータ及びマルチパルスガスジェネレータの動作方法
CN112855385B (zh) * 2021-01-08 2022-03-29 西安近代化学研究所 一种适用于低温点火的装药结构
CN113153572A (zh) * 2021-03-31 2021-07-23 西北工业大学 一种弧形叶片固体火箭发动机药柱结构
US11846252B2 (en) 2021-09-03 2023-12-19 Raytheon Company Propulsion system with initiators for selective activation of multiple rocket motors
US11643997B2 (en) * 2021-09-03 2023-05-09 Raytheon Company Propulsion system with single initiator for multiple rocket motors
US11852104B2 (en) 2021-09-03 2023-12-26 Raytheon Company Propulsion system with single initiator for multiple rocket motors

Also Published As

Publication number Publication date
BE726920A (xx) 1969-06-16
GB1216823A (en) 1970-12-23
SE336933B (xx) 1971-07-19
FR1600673A (xx) 1970-07-27
US3555825A (en) 1971-01-19
DE1626079A1 (de) 1971-03-11

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