US3921937A - Projectile or rocket preferably with unfolded tail unit - Google Patents

Projectile or rocket preferably with unfolded tail unit Download PDF

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Publication number
US3921937A
US3921937A US366755A US36675573A US3921937A US 3921937 A US3921937 A US 3921937A US 366755 A US366755 A US 366755A US 36675573 A US36675573 A US 36675573A US 3921937 A US3921937 A US 3921937A
Authority
US
United States
Prior art keywords
disk
sliding sleeve
projectile
rudder carrier
annular
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
US366755A
Other languages
English (en)
Inventor
Alfred Voss
Manfred Strunk
Heinz Kroschel
Heinz Wilhelm Kreutz
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
Application granted granted Critical
Publication of US3921937A publication Critical patent/US3921937A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
US366755A 1972-06-03 1973-06-04 Projectile or rocket preferably with unfolded tail unit Expired - Lifetime US3921937A (en)

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 (1)

Publication Number Publication Date
US3921937A true US3921937A (en) 1975-11-25

Family

ID=5846743

Family Applications (1)

Application Number Title Priority Date Filing Date
US366755A Expired - Lifetime US3921937A (en) 1972-06-03 1973-06-04 Projectile or rocket preferably with unfolded tail unit

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)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4296894A (en) * 1979-02-08 1981-10-27 Messerschmitt-Bolkow-Blohm Gmbh Drone-type missile
US4600167A (en) * 1983-08-06 1986-07-15 Diehl Gmbh & Co. Pivoting guidance mechanism for small-calibered projectiles
US5671899A (en) * 1996-02-26 1997-09-30 Lockheed Martin Corporation Airborne vehicle with wing extension and roll control
US6398156B2 (en) * 1999-12-16 2002-06-04 Lfk Lenkflugkoerpersysteme Gmbh Mounting for attaching a rudder to a missile
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
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
US20140312575A1 (en) * 2010-04-07 2014-10-23 William D. Barry Wing slot seal
CN108801078A (zh) * 2018-08-23 2018-11-13 中国工程物理研究院总体工程研究所 杀爆火箭弹
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)
US11340052B2 (en) 2019-08-27 2022-05-24 Bae Systems Information And Electronic Systems Integration Inc. Wing deployment initiator and locking mechanism
US11852211B2 (en) 2020-09-10 2023-12-26 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured elliptical bifurcating torsion spring

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3227766C1 (de) * 1982-07-24 1988-01-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Gefechtskopf
DE3507677A1 (de) * 1985-03-05 1986-09-11 Diehl GmbH & Co, 8500 Nürnberg Flugkoerper mit ueberkalibrigem leitwerk
DE10015514B4 (de) * 2000-03-30 2007-10-04 Rheinmetall Waffe Munition Gmbh Flügelstabilisiertes Geschoß
DE202009016713U1 (de) 2009-12-04 2010-04-08 Lehnen, Frank Widerstandsstabilisiertes, flügelloses und angetriebenes Wuchtgeschoss
DE102009057682A1 (de) 2009-12-04 2011-06-09 Frank Lehnen Widerstandsstabilisiertes, flügelloses und angetriebenes Wuchtgeschoss

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3119335A (en) * 1960-03-03 1964-01-28 Brevets Aero Mecaniques Projectiles fitted with and electric detonator operated by a generator of the inertia type
US3289587A (en) * 1965-07-07 1966-12-06 John J Donnelly Fin stabilized projectile
US3598345A (en) * 1967-09-06 1971-08-10 Oerlikon Buehrle Ag Rocket with folding fins and braking device

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1198248B (de) * 1963-07-17 1965-08-05 Diehl Fa Klappleitwerk
DE1428669A1 (de) * 1963-11-14 1968-12-05 Diehl Fa Klappleitwerk
CH481364A (de) * 1967-09-21 1969-11-15 Oerlikon Buehrle Ag Rakete mit aufklappbarem Leitwerk

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3119335A (en) * 1960-03-03 1964-01-28 Brevets Aero Mecaniques Projectiles fitted with and electric detonator operated by a generator of the inertia type
US3289587A (en) * 1965-07-07 1966-12-06 John J Donnelly Fin stabilized projectile
US3598345A (en) * 1967-09-06 1971-08-10 Oerlikon Buehrle Ag Rocket with folding fins and braking device

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4296894A (en) * 1979-02-08 1981-10-27 Messerschmitt-Bolkow-Blohm Gmbh Drone-type missile
US4600167A (en) * 1983-08-06 1986-07-15 Diehl Gmbh & Co. Pivoting guidance mechanism for small-calibered projectiles
US5671899A (en) * 1996-02-26 1997-09-30 Lockheed Martin Corporation Airborne vehicle with wing extension and roll control
US6398156B2 (en) * 1999-12-16 2002-06-04 Lfk Lenkflugkoerpersysteme Gmbh Mounting for attaching a rudder to a missile
US8895908B2 (en) * 2010-04-07 2014-11-25 Bae Systems Information And Electronic Systems Integration Inc. Wing slot seal
US20140312575A1 (en) * 2010-04-07 2014-10-23 William D. Barry Wing slot seal
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
US20120074256A1 (en) * 2010-04-07 2012-03-29 Amy Pietrzak Compression spring wing deployment initiator
WO2011126970A3 (fr) * 2010-04-07 2012-04-19 Bae Systems Information And Electronic Systems Integration Inc. Initiateur de déploiement d'aile à ressort de compression
US8754352B2 (en) * 2010-04-07 2014-06-17 Bae Systems Information And Electronic Systems Integration Inc. Compression spring wing deployment initiator
US8686329B2 (en) 2010-04-09 2014-04-01 Bae Systems Information And Electronic Systems Integration Inc. Torsion spring wing deployment initiator
WO2011127369A3 (fr) * 2010-04-09 2012-02-23 Bae Systems Information And Electronic Systems Integration Inc. Déclencheur de déploiement d'aile à ressorts de torsion
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
CN108801078A (zh) * 2018-08-23 2018-11-13 中国工程物理研究院总体工程研究所 杀爆火箭弹
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

Also Published As

Publication number Publication date
DE2227104A1 (de) 1973-12-13
FR2188137B1 (fr) 1977-12-30
DE2227104C2 (de) 1982-07-15
GB1422987A (en) 1976-01-28
FR2188137A1 (fr) 1974-01-18
IT985639B (it) 1974-12-10
BE800259A (fr) 1973-09-17

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