DE59502739D1 - Schuberzeugungsvorrichtung - Google Patents

Schuberzeugungsvorrichtung

Info

Publication number
DE59502739D1
DE59502739D1 DE59502739T DE59502739T DE59502739D1 DE 59502739 D1 DE59502739 D1 DE 59502739D1 DE 59502739 T DE59502739 T DE 59502739T DE 59502739 T DE59502739 T DE 59502739T DE 59502739 D1 DE59502739 D1 DE 59502739D1
Authority
DE
Germany
Prior art keywords
generating device
thrust generating
thrust
generating
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
DE59502739T
Other languages
English (en)
Inventor
Wolfgang Ing Mueller
German Dipl Ing Munding
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.)
Airbus Defence and Space GmbH
Original Assignee
Daimler Benz Aerospace AG
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 Daimler Benz Aerospace AG filed Critical Daimler Benz Aerospace AG
Application granted granted Critical
Publication of DE59502739D1 publication Critical patent/DE59502739D1/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
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
DE59502739T 1994-04-30 1995-04-27 Schuberzeugungsvorrichtung Expired - Lifetime DE59502739D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4415259A DE4415259C1 (de) 1994-04-30 1994-04-30 Schuberzeugungsvorrichtung

Publications (1)

Publication Number Publication Date
DE59502739D1 true DE59502739D1 (de) 1998-08-13

Family

ID=6516952

Family Applications (2)

Application Number Title Priority Date Filing Date
DE4415259A Expired - Fee Related DE4415259C1 (de) 1994-04-30 1994-04-30 Schuberzeugungsvorrichtung
DE59502739T Expired - Lifetime DE59502739D1 (de) 1994-04-30 1995-04-27 Schuberzeugungsvorrichtung

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE4415259A Expired - Fee Related DE4415259C1 (de) 1994-04-30 1994-04-30 Schuberzeugungsvorrichtung

Country Status (3)

Country Link
US (1) US5661970A (de)
EP (1) EP0686824B1 (de)
DE (2) DE4415259C1 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6131385A (en) * 1997-08-18 2000-10-17 Trw Inc. Integrated pulsed propulsion system for microsatellite
US6158693A (en) * 1998-02-25 2000-12-12 Kistler Aerospace Corporation Recoverable booster stage and recovery method
US6487844B1 (en) * 1999-11-24 2002-12-03 Trw Inc. Aerospike augmentation of microthruster impulse
NO20002377A (no) * 2000-05-05 2001-06-25 Nammo Raufoss As Anordning ved beholder som omslutter et brennbart materiale
US6494402B2 (en) * 2001-05-14 2002-12-17 The Aerospace Corporation Lateral exhaust microthruster
US7273352B2 (en) * 2004-01-09 2007-09-25 United Technologies Corporation Inlet partial blades for structural integrity and performance
US20110008327A1 (en) * 2004-03-29 2011-01-13 Cheng Jin Q Compositions including triciribine and epidermal growth factor receptor inhibitor compounds or salts thereof and methods of use thereof
US20070295857A1 (en) * 2005-11-16 2007-12-27 Lloyd Peter G Emergency Device
US9404441B2 (en) * 2008-08-18 2016-08-02 Aerojet Rocketdyne Of De, Inc. Low velocity injector manifold for hypergolic rocket engine
US20110116934A1 (en) * 2009-11-16 2011-05-19 Meng Sen Y Pumping element design
CN110510128B (zh) * 2019-08-02 2021-04-20 宁波天擎航天科技有限公司 一种推进系统
CN113154957B (zh) * 2021-04-15 2022-09-16 湖北航天技术研究院总体设计所 一种火箭方舱装置及其使用方法
CN114576041A (zh) * 2022-02-10 2022-06-03 宁波天擎航天科技有限公司 一种高集成阀门及控制系统
CN117028076B (zh) * 2023-10-09 2024-01-09 北京星河动力装备科技有限公司 火箭发动机的启动方法和火箭

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3098625A (en) * 1960-12-19 1963-07-23 Thompson Ramo Wooldridge Inc Rocket motor and control system
US3098353A (en) * 1961-03-31 1963-07-23 United Aircraft Corp Rocket engine propellant feeding and control system
US3842598A (en) * 1966-11-09 1974-10-22 Us Army Rocket power plant
DE2057326C3 (de) * 1970-11-21 1980-01-24 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt Flüssigkeits-Raketentriebwerk
US3736749A (en) * 1971-08-20 1973-06-05 Lockheed Missiles Space Open loop on-demand variable flow gas generator system with a two-position injector
EP0060726A3 (de) * 1981-03-17 1983-02-09 Normalair-Garrett (Holdings) Limited Strahltrieb-Schubsysteme
DE3521204A1 (de) * 1985-06-13 1986-12-18 Diehl GmbH & Co, 8500 Nürnberg Impulstriebwerk
DE3531686A1 (de) * 1985-09-05 1987-03-12 Rheinmetall Gmbh Steuerblock
US4899956A (en) * 1988-07-20 1990-02-13 Teleflex, Incorporated Self-contained supplemental guidance module for projectile weapons

Also Published As

Publication number Publication date
EP0686824A1 (de) 1995-12-13
EP0686824B1 (de) 1998-07-08
DE4415259C1 (de) 1995-06-08
US5661970A (en) 1997-09-02

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: DAIMLERCHRYSLER AEROSPACE AKTIENGESELLSCHAFT, 8099

8327 Change in the person/name/address of the patent owner

Owner name: DAIMLERCHRYSLER AEROSPACE AG, 85521 OTTOBRUNN, DE