FR2188137B1 - - Google Patents

Info

Publication number
FR2188137B1
FR2188137B1 FR7319556A FR7319556A FR2188137B1 FR 2188137 B1 FR2188137 B1 FR 2188137B1 FR 7319556 A FR7319556 A FR 7319556A FR 7319556 A FR7319556 A FR 7319556A FR 2188137 B1 FR2188137 B1 FR 2188137B1
Authority
FR
France
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
Application number
FR7319556A
Other versions
FR2188137A1 (fr
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.)
Dynamit Nobel AG
Original Assignee
Dynamit Nobel 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 Dynamit Nobel AG filed Critical Dynamit Nobel AG
Publication of FR2188137A1 publication Critical patent/FR2188137A1/fr
Application granted granted Critical
Publication of FR2188137B1 publication Critical patent/FR2188137B1/fr
Expired 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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces
FR7319556A 1972-06-03 1973-05-29 Expired FR2188137B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2227104A DE2227104C2 (de) 1972-06-03 1972-06-03 Geschoß oder Rakete mit aufklappbarem Leitwerk

Publications (2)

Publication Number Publication Date
FR2188137A1 FR2188137A1 (fr) 1974-01-18
FR2188137B1 true FR2188137B1 (fr) 1977-12-30

Family

ID=5846743

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7319556A Expired FR2188137B1 (fr) 1972-06-03 1973-05-29

Country Status (6)

Country Link
US (1) US3921937A (fr)
BE (1) BE800259A (fr)
DE (1) DE2227104C2 (fr)
FR (1) FR2188137B1 (fr)
GB (1) GB1422987A (fr)
IT (1) IT985639B (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2904749C2 (de) * 1979-02-08 1984-01-05 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flugkörper nach Art einer Drohne
DE3227766C1 (de) * 1982-07-24 1988-01-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Gefechtskopf
DE3328520C1 (de) * 1983-08-06 1985-03-07 Diehl GmbH & Co, 8500 Nürnberg Schwenkleitwerk fuer Flugkoerper
DE3507677A1 (de) * 1985-03-05 1986-09-11 Diehl GmbH & Co, 8500 Nürnberg Flugkoerper mit ueberkalibrigem leitwerk
US5671899A (en) * 1996-02-26 1997-09-30 Lockheed Martin Corporation Airborne vehicle with wing extension and roll control
DE19960738C1 (de) * 1999-12-16 2001-08-23 Lfk Gmbh Ruderanbindung für Lenkflugkörper
DE10015514B4 (de) * 2000-03-30 2007-10-04 Rheinmetall Waffe Munition Gmbh Flügelstabilisiertes Geschoß
DE102009057682A1 (de) 2009-12-04 2011-06-09 Frank Lehnen Widerstandsstabilisiertes, flügelloses und angetriebenes Wuchtgeschoss
DE202009016713U1 (de) 2009-12-04 2010-04-08 Lehnen, Frank Widerstandsstabilisiertes, flügelloses und angetriebenes Wuchtgeschoss
WO2011126970A2 (fr) * 2010-04-07 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Initiateur de déploiement d'aile à ressort de compression
WO2012003025A2 (fr) * 2010-04-07 2012-01-05 Bae Systems Information And Electronic Systems Integration Inc. Joint d'étanchéité de fente d'aile
WO2011127369A2 (fr) * 2010-04-09 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Déclencheur de déploiement d'aile à ressorts de torsion
CN108801078B (zh) * 2018-08-23 2024-02-27 中国工程物理研究院总体工程研究所 杀爆火箭弹
US11340052B2 (en) 2019-08-27 2022-05-24 Bae Systems Information And Electronic Systems Integration Inc. Wing deployment initiator and locking mechanism
US20220011082A1 (en) * 2020-07-10 2022-01-13 Pneu-Dart Tail Piece for Remote Delivery Device ( CIP of Application 15/932.942 filed 05/24/2018)
US11852211B2 (en) 2020-09-10 2023-12-26 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured elliptical bifurcating torsion spring

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL121387C (fr) * 1960-03-03
DE1198248B (de) * 1963-07-17 1965-08-05 Diehl Fa Klappleitwerk
DE1428669A1 (de) * 1963-11-14 1968-12-05 Diehl Fa Klappleitwerk
US3289587A (en) * 1965-07-07 1966-12-06 John J Donnelly Fin stabilized projectile
CH480612A (de) * 1967-09-06 1969-10-31 Oerlikon Buehrle Ag Rakete mit Klappleitwerk und Bremsvorrichtung
CH481364A (de) * 1967-09-21 1969-11-15 Oerlikon Buehrle Ag Rakete mit aufklappbarem Leitwerk

Also Published As

Publication number Publication date
BE800259A (fr) 1973-09-17
US3921937A (en) 1975-11-25
GB1422987A (en) 1976-01-28
FR2188137A1 (fr) 1974-01-18
IT985639B (it) 1974-12-10
DE2227104A1 (de) 1973-12-13
DE2227104C2 (de) 1982-07-15

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Legal Events

Date Code Title Description
ST Notification of lapse