IT985639B - BULLET OR ROCKET WITH HINGED OPENING DIRECTIVE FINS - Google Patents

BULLET OR ROCKET WITH HINGED OPENING DIRECTIVE FINS

Info

Publication number
IT985639B
IT985639B IT50360/73A IT5036073A IT985639B IT 985639 B IT985639 B IT 985639B IT 50360/73 A IT50360/73 A IT 50360/73A IT 5036073 A IT5036073 A IT 5036073A IT 985639 B IT985639 B IT 985639B
Authority
IT
Italy
Prior art keywords
rocket
bullet
fins
hinged opening
opening directive
Prior art date
Application number
IT50360/73A
Other languages
Italian (it)
Inventor
M Strunk
H Kroschel
A Voss
H Kreutz
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 IT985639B publication Critical patent/IT985639B/en

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
IT50360/73A 1972-06-03 1973-06-01 BULLET OR ROCKET WITH HINGED OPENING DIRECTIVE FINS IT985639B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2227104A DE2227104C2 (en) 1972-06-03 1972-06-03 Projectile or missile with a hinged tail unit

Publications (1)

Publication Number Publication Date
IT985639B true IT985639B (en) 1974-12-10

Family

ID=5846743

Family Applications (1)

Application Number Title Priority Date Filing Date
IT50360/73A IT985639B (en) 1972-06-03 1973-06-01 BULLET OR ROCKET WITH HINGED OPENING DIRECTIVE FINS

Country Status (6)

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

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2904749C2 (en) * 1979-02-08 1984-01-05 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Missile in the manner of a drone
DE3227766C1 (en) * 1982-07-24 1988-01-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Warhead
DE3328520C1 (en) * 1983-08-06 1985-03-07 Diehl GmbH & Co, 8500 Nürnberg Tailplane for missiles
DE3507677A1 (en) * 1985-03-05 1986-09-11 Diehl GmbH & Co, 8500 Nürnberg MISSILE WITH OVER-CALIBRATE ANALYSIS
US5671899A (en) * 1996-02-26 1997-09-30 Lockheed Martin Corporation Airborne vehicle with wing extension and roll control
DE19960738C1 (en) * 1999-12-16 2001-08-23 Lfk Gmbh Rudder connection for guided missiles
DE10015514B4 (en) * 2000-03-30 2007-10-04 Rheinmetall Waffe Munition Gmbh Wing stabilized projectile
DE102009057682A1 (en) 2009-12-04 2011-06-09 Frank Lehnen Kinetic energy projectile i.e. caseless munition, has drive and resistance stabilizer for firing of smooth or profiled gun tubes, where projectile exhibits rotation symmetric tail-shape at longitudinal axis
DE202009016713U1 (en) 2009-12-04 2010-04-08 Lehnen, Frank Resistance-stabilized, wingless and powered balancing projectile
WO2011126970A2 (en) * 2010-04-07 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Compression spring wing deployment initiator
WO2012003025A2 (en) * 2010-04-07 2012-01-05 Bae Systems Information And Electronic Systems Integration Inc. Wing slot seal
WO2011127369A2 (en) * 2010-04-09 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Torsion spring wing deployment initiator
CN108801078B (en) * 2018-08-23 2024-02-27 中国工程物理研究院总体工程研究所 Explosion-proof rocket projectile
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 (en) * 1960-03-03
DE1198248B (en) * 1963-07-17 1965-08-05 Diehl Fa Folding tail
DE1428669A1 (en) * 1963-11-14 1968-12-05 Diehl Fa Folding tail
US3289587A (en) * 1965-07-07 1966-12-06 John J Donnelly Fin stabilized projectile
CH480612A (en) * 1967-09-06 1969-10-31 Oerlikon Buehrle Ag Rocket with folding tail and braking device
CH481364A (en) * 1967-09-21 1969-11-15 Oerlikon Buehrle Ag Rocket with a hinged tail unit

Also Published As

Publication number Publication date
BE800259A (en) 1973-09-17
US3921937A (en) 1975-11-25
FR2188137B1 (en) 1977-12-30
GB1422987A (en) 1976-01-28
FR2188137A1 (en) 1974-01-18
DE2227104A1 (en) 1973-12-13
DE2227104C2 (en) 1982-07-15

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