CH469242A - Projectile - Google Patents
ProjectileInfo
- Publication number
- CH469242A CH469242A CH863667A CH863667A CH469242A CH 469242 A CH469242 A CH 469242A CH 863667 A CH863667 A CH 863667A CH 863667 A CH863667 A CH 863667A CH 469242 A CH469242 A CH 469242A
- Authority
- CH
- Switzerland
- Prior art keywords
- projectile
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/22—Homing guidance systems
- F41G7/222—Homing guidance systems for spin-stabilized missiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/30—Command link guidance systems
- F41G7/301—Details
- F41G7/305—Details for spin-stabilized missiles
-
- 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
- F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE683586 | 1966-07-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH469242A true CH469242A (fr) | 1969-02-28 |
Family
ID=3849029
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH863667A CH469242A (fr) | 1966-07-04 | 1967-06-19 | Projectile |
Country Status (9)
Country | Link |
---|---|
US (1) | US3398916A (fr) |
AT (1) | AT278594B (fr) |
BE (1) | BE683586A (fr) |
CH (1) | CH469242A (fr) |
ES (1) | ES342471A1 (fr) |
GB (1) | GB1193304A (fr) |
IL (1) | IL28154A (fr) |
NL (1) | NL6708669A (fr) |
SE (1) | SE348829B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU1841351C (ru) * | 1970-03-27 | 2023-07-31 | Акционерное общество "Центральный научно-исследовательский радиотехнический институт имени академика А.И. Берга" | Конструкция ориентированной с помощью вращения головной части ракеты |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2091901B2 (fr) * | 1970-04-10 | 1973-12-21 | Etu Realisa Electronique | |
CA1009370A (en) * | 1972-01-03 | 1977-04-26 | Ship Systems | Laser guided projectile |
DE2741984C2 (de) * | 1977-09-17 | 1984-01-26 | Franz Rudolf Prof.Dr.Dipl.-Ing. West Vancouver Thomanek | Gefechtskopf für einen Panzerabwehrflugkörper mit mindestens einer stachelbildenden Hohlladung |
US4160415A (en) * | 1978-05-05 | 1979-07-10 | The United States Of America As Represented By The Secretary Of The Army | Target activated projectile |
USRE32094E (en) * | 1979-11-09 | 1986-03-25 | Avco Corporation | Overflying munitions device and system |
GB2370342B (en) * | 1981-11-05 | 2002-11-20 | Emi Ltd | Terminally - corrected sub-munitions |
CA1242516A (fr) * | 1982-04-21 | 1988-09-27 | William H. Bell | Systeme d'orme a guidage jusqu'au point d'impact |
GB2251834B (en) * | 1983-02-22 | 1992-12-16 | George Alexander Tarrant | Guided missiles |
DE3345529C1 (de) * | 1983-12-16 | 1999-09-02 | Diehl Stiftung & Co | Zielsuchende Munition mit vor ihrer Gefechtsladung-Einlage angeordnetem Sensor-Wandler |
DE3911576A1 (de) * | 1989-04-08 | 1990-10-11 | Rheinmetall Gmbh | Fluegelstabilisiertes geschoss |
US5261629A (en) * | 1989-04-08 | 1993-11-16 | Rheinmetall Gmbh | Fin stabilized projectile |
GB2250804B (en) * | 1990-11-07 | 1994-06-01 | Colebrand Ltd | Protective device for a sensing head |
DE4210113C1 (de) * | 1992-03-27 | 1998-11-05 | Athanassios Dr Ing Zacharias | Verfahren zum Leiten eines Flugkörpers und Flugkörper |
US6722609B2 (en) * | 1998-02-13 | 2004-04-20 | James M. Linick | Impulse motor and apparatus to improve trajectory correctable munitions including cannon launched munitions, glide bombs, missiles, rockets and the like |
WO2000052414A1 (fr) * | 1999-03-03 | 2000-09-08 | Linick James M | Moteur a impulsions visant a ameliorer des munitions a trajectoires rectifiables |
US6502785B1 (en) * | 1999-11-17 | 2003-01-07 | Lockheed Martin Corporation | Three axis flap control system |
AU1013002A (en) * | 2000-05-25 | 2001-12-03 | Metal Storm Ltd | Directional control of missiles |
AUPQ776300A0 (en) | 2000-05-25 | 2000-08-10 | Metal Storm Limited | Missile control |
US6994294B2 (en) * | 2003-08-29 | 2006-02-07 | Smiths Aerospace, Inc. | Stabilization of a drogue body |
US7377468B2 (en) * | 2003-08-29 | 2008-05-27 | Smiths Aerospace Llc | Active stabilization of a refueling drogue |
US7681839B2 (en) * | 2005-02-25 | 2010-03-23 | Smiths Aerospace Llc | Optical tracking system for refueling |
US8084725B1 (en) * | 2008-05-01 | 2011-12-27 | Raytheon Company | Methods and apparatus for fast action impulse thruster |
RU2443968C2 (ru) * | 2009-03-19 | 2012-02-27 | Николай Евгеньевич Староверов | Противовертолетная и противостелсовая ракета |
US10615547B2 (en) | 2016-09-08 | 2020-04-07 | Raytheon Company | Electrical device with shunt, and receptacle |
US10662898B2 (en) | 2016-09-08 | 2020-05-26 | Raytheon Company | Integrated thruster |
CN112199635B (zh) * | 2020-10-17 | 2024-03-29 | 中国人民解放军63876部队 | 一种火箭橇运动弹道计算修正方法 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2029491A (en) * | 1934-08-25 | 1936-02-04 | Technicraft Engineering Corp | Gun type formation tester |
US2258281A (en) * | 1938-05-20 | 1941-10-07 | Commercial Ingredients Corp | Aerial torpedo |
NL228838A (fr) * | 1957-06-19 | |||
US3107617A (en) * | 1962-04-11 | 1963-10-22 | William F Loeper | Ring decoy launching mechanism |
-
1966
- 1966-07-04 BE BE683586D patent/BE683586A/xx unknown
-
1967
- 1967-06-18 IL IL28154A patent/IL28154A/en unknown
- 1967-06-19 CH CH863667A patent/CH469242A/fr unknown
- 1967-06-19 US US646899A patent/US3398916A/en not_active Expired - Lifetime
- 1967-06-19 SE SE08649/67A patent/SE348829B/xx unknown
- 1967-06-19 AT AT569667A patent/AT278594B/de not_active IP Right Cessation
- 1967-06-21 NL NL6708669A patent/NL6708669A/xx unknown
- 1967-06-21 GB GB28551/67A patent/GB1193304A/en not_active Expired
- 1967-06-30 ES ES342471A patent/ES342471A1/es not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU1841351C (ru) * | 1970-03-27 | 2023-07-31 | Акционерное общество "Центральный научно-исследовательский радиотехнический институт имени академика А.И. Берга" | Конструкция ориентированной с помощью вращения головной части ракеты |
Also Published As
Publication number | Publication date |
---|---|
US3398916A (en) | 1968-08-27 |
ES342471A1 (es) | 1968-07-16 |
AT278594B (de) | 1970-02-10 |
DE1578139B1 (de) | 1971-12-23 |
NL6708669A (fr) | 1968-01-05 |
GB1193304A (en) | 1970-05-28 |
BE683586A (fr) | 1966-12-16 |
IL28154A (en) | 1972-08-30 |
SE348829B (fr) | 1972-09-11 |
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