NO161463C - Hurtigflyvende legeme. - Google Patents
Hurtigflyvende legeme.Info
- Publication number
- NO161463C NO161463C NO871505A NO871505A NO161463C NO 161463 C NO161463 C NO 161463C NO 871505 A NO871505 A NO 871505A NO 871505 A NO871505 A NO 871505A NO 161463 C NO161463 C NO 161463C
- Authority
- NO
- Norway
- Prior art keywords
- flying body
- fast flying
- fast
- flying
- Prior art date
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
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/42—Streamlined projectiles
- F42B10/46—Streamlined nose cones; Windshields; Radomes
-
- 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
- F42B10/62—Steering by movement of flight surfaces
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
- Escalators And Moving Walkways (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3612175A DE3612175C1 (de) | 1986-04-11 | 1986-04-11 | Schnellfliegender Flugkoerper |
Publications (4)
Publication Number | Publication Date |
---|---|
NO871505D0 NO871505D0 (no) | 1987-04-10 |
NO871505L NO871505L (no) | 1987-10-12 |
NO161463B NO161463B (no) | 1989-05-08 |
NO161463C true NO161463C (no) | 1989-08-16 |
Family
ID=6298446
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO871505A NO161463C (no) | 1986-04-11 | 1987-04-10 | Hurtigflyvende legeme. |
Country Status (4)
Country | Link |
---|---|
US (1) | US4756492A (no) |
EP (1) | EP0249677B1 (no) |
DE (1) | DE3612175C1 (no) |
NO (1) | NO161463C (no) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4998994A (en) * | 1989-09-20 | 1991-03-12 | The United States Of America As Represented By The Secretary Of The Army | Aerodynamically compliant projectile nose |
GB8925397D0 (en) * | 1989-11-10 | 1992-11-04 | Secr Defence | Kinetic energy penetrator |
DE4239589A1 (de) * | 1992-11-25 | 1994-05-26 | Deutsche Aerospace | Vorrichtung zum Steuern von Flugkörpern mit einem aerodynamisch wirkenden Steuerkörper |
US5794887A (en) * | 1995-11-17 | 1998-08-18 | Komerath; Narayanan M. | Stagnation point vortex controller |
FR2761769B1 (fr) * | 1997-04-08 | 1999-07-02 | Tda Armements Sas | Dispositif de microgouverne pour la correction de trajectoire de munition stabilisee par rotation |
US6389977B1 (en) * | 1997-12-11 | 2002-05-21 | Lockheed Martin Corporation | Shrouded aerial bomb |
US6845718B2 (en) | 2002-12-18 | 2005-01-25 | Lockheed Martin Corporation | Projectile capable of propelling a penetrator therefrom and method of using same |
US6796532B2 (en) * | 2002-12-20 | 2004-09-28 | Norman D. Malmuth | Surface plasma discharge for controlling forebody vortex asymmetry |
DE102006003638B4 (de) | 2006-01-26 | 2008-01-17 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flugkörper für den Überschallbereich |
US7834301B2 (en) * | 2008-04-30 | 2010-11-16 | The Boeing Company | System and method for controlling high spin rate projectiles |
IL210370A (en) * | 2010-12-30 | 2015-08-31 | Israel Aerospace Ind Ltd | missile |
CN102167162A (zh) * | 2011-03-10 | 2011-08-31 | 洪瑞庆 | 一种用于飞行器的超高压流体喷射动力变轨系统及方法 |
US9132908B1 (en) * | 2013-03-15 | 2015-09-15 | The Boeing Company | Expandable nose cone |
US10928169B2 (en) * | 2019-02-07 | 2021-02-23 | Bae Systems Rokar International Ltd. | Seal for a projectile guiding kit |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3067682A (en) * | 1960-02-18 | 1962-12-11 | Aerojet General Co | Gyro pull rocket |
US3195462A (en) * | 1961-05-17 | 1965-07-20 | Aerojet General Co | Pull rocket shroud |
US3262655A (en) * | 1963-12-26 | 1966-07-26 | Jr Warren Gillespie | Alleviation of divergence during rocket launch |
US3292879A (en) * | 1965-06-25 | 1966-12-20 | Canrad Prec Ind Inc | Projectile with stabilizing surfaces |
IL46548A (en) * | 1975-02-03 | 1978-06-15 | Drori Mordeki | Stabilized projectile with pivotable fins |
WO1982003453A1 (en) * | 1981-04-08 | 1982-10-14 | Thomson Keith Donald | Directional control device for airborne or seaborne missiles |
US4399962A (en) * | 1981-08-31 | 1983-08-23 | General Dynamics, Pomona Division | Wobble nose control for projectiles |
DE3347005A1 (de) * | 1983-12-24 | 1985-07-04 | Dynamit Nobel Ag, 5210 Troisdorf | Flugkoerper |
-
1986
- 1986-04-11 DE DE3612175A patent/DE3612175C1/de not_active Expired
-
1987
- 1987-01-28 EP EP87101159A patent/EP0249677B1/de not_active Expired - Lifetime
- 1987-03-31 US US07/032,747 patent/US4756492A/en not_active Expired - Fee Related
- 1987-04-10 NO NO871505A patent/NO161463C/no unknown
Also Published As
Publication number | Publication date |
---|---|
EP0249677A1 (de) | 1987-12-23 |
NO161463B (no) | 1989-05-08 |
EP0249677B1 (de) | 1990-05-09 |
DE3612175C1 (de) | 1987-10-08 |
NO871505L (no) | 1987-10-12 |
US4756492A (en) | 1988-07-12 |
NO871505D0 (no) | 1987-04-10 |
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