CH479849A - Porietto autopropulso o semiautopropulso con governale ad alette retrattili - Google Patents
Porietto autopropulso o semiautopropulso con governale ad alette retrattiliInfo
- Publication number
- CH479849A CH479849A CH942568A CH942568A CH479849A CH 479849 A CH479849 A CH 479849A CH 942568 A CH942568 A CH 942568A CH 942568 A CH942568 A CH 942568A CH 479849 A CH479849 A CH 479849A
- Authority
- CH
- Switzerland
- Prior art keywords
- propelled
- self
- porietto
- governor
- semi
- 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
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Support Of The Bearing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Rolling Contact Bearings (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT3836067 | 1967-07-22 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CH479849A true CH479849A (it) | 1969-10-15 |
Family
ID=11246023
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH942568A CH479849A (it) | 1967-07-22 | 1968-06-24 | Porietto autopropulso o semiautopropulso con governale ad alette retrattili |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3602459A (it) |
| CH (1) | CH479849A (it) |
| DE (1) | DE1703722C3 (it) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1995031689A1 (en) * | 1994-05-13 | 1995-11-23 | Hughes Aircraft Company | Missile with deployable control fins |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2041502B (en) * | 1979-02-08 | 1982-09-08 | British Aerospace | Folding fin assembly |
| US4364531A (en) * | 1980-10-09 | 1982-12-21 | Knoski Jerry L | Attachable airfoil with movable control surface |
| DE3515326A1 (de) * | 1985-04-27 | 1986-10-30 | Rheinmetall GmbH, 4000 Düsseldorf | Nutzlastgeschoss |
| SE460436B (sv) * | 1986-12-01 | 1989-10-09 | Bofors Ab | Anordning foer att minska rotationen och samtidigt aastadkomma en sidohastighet hos en roterande ammunitionsenhet |
| IL101730A (en) * | 1992-04-30 | 1995-12-31 | Israel State | Moving body such as missile having wings erectable upon acceleration |
| US6168111B1 (en) * | 1997-03-03 | 2001-01-02 | The United States Of America As Represented By The Secretary Of The Army | Fold-out fin |
| US8816261B1 (en) * | 2011-06-29 | 2014-08-26 | Raytheon Company | Bang-bang control using tangentially mounted surfaces |
| WO2018015838A1 (en) * | 2016-07-21 | 2018-01-25 | Chairman, Defence Research &Development Organisation (Drdo) | Bi-directional wing unfolding mechanism |
| US11187505B1 (en) * | 2019-07-03 | 2021-11-30 | Gerhard W. Thielman | Concatenated annular swing-wing tandem lift enhancer |
| US20250334386A1 (en) * | 2024-01-10 | 2025-10-30 | U.S. Army DEVCOM Army Research Laboratory | Deploying fins for a gun-launched projectile |
-
1968
- 1968-06-24 CH CH942568A patent/CH479849A/it not_active IP Right Cessation
- 1968-07-03 DE DE1703722A patent/DE1703722C3/de not_active Expired
-
1969
- 1969-07-14 US US871448*A patent/US3602459A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1995031689A1 (en) * | 1994-05-13 | 1995-11-23 | Hughes Aircraft Company | Missile with deployable control fins |
Also Published As
| Publication number | Publication date |
|---|---|
| US3602459A (en) | 1971-08-31 |
| DE1703722C3 (de) | 1974-04-04 |
| DE1703722A1 (de) | 1972-04-27 |
| DE1703722B2 (de) | 1973-09-06 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PL | Patent ceased |