GB1386350A - Rockers with finned tail-unit - Google Patents
Rockers with finned tail-unitInfo
- Publication number
- GB1386350A GB1386350A GB1113472A GB1113472A GB1386350A GB 1386350 A GB1386350 A GB 1386350A GB 1113472 A GB1113472 A GB 1113472A GB 1113472 A GB1113472 A GB 1113472A GB 1386350 A GB1386350 A GB 1386350A
- Authority
- GB
- United Kingdom
- Prior art keywords
- studs
- received
- rocket
- during launch
- guide
- 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
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
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
1386350 Projectiles; rocket launcher CONSTRUCTIONS NAVALES ET INDUSTRIELLES DE LA MEDITERRANEE 9 March 1972 [29 March 1971] 11134/72 Headings F3A and F3C A rocket comprises: a body 1; two or more first studs 5 to be received in a helical guide for rotating the body during launch; a fin unit 9 mounted on the body for relative rotation and having two or more studs 8 to be received in rectilinear guides for preventing rotation of the fin unit during launch; and two or more third studs 6 mounted for rotational movement relative to the body 1 to be received in a rectilinear guide to guide the rocket during launch. The studs 6 are affixed to a collar 7 rotatable relative to the body 1. In another embodiment (Fig. 2, not shown), the second and third studs are affixed to a tubular extension (9) of the tail piece.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7110894A FR2130968A5 (en) | 1971-03-29 | 1971-03-29 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1386350A true GB1386350A (en) | 1975-03-05 |
Family
ID=9074267
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1113472A Expired GB1386350A (en) | 1971-03-29 | 1972-03-09 | Rockers with finned tail-unit |
Country Status (7)
| Country | Link |
|---|---|
| CA (1) | CA956839A (en) |
| CH (1) | CH567708A5 (en) |
| FR (1) | FR2130968A5 (en) |
| GB (1) | GB1386350A (en) |
| IL (1) | IL38967A (en) |
| IT (1) | IT950409B (en) |
| ZA (1) | ZA721701B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2924217A1 (en) * | 1979-06-15 | 1980-12-18 | Rheinmetall Gmbh | Sub calibre shell for firing practice - has spin caused by released vaned adaptor opposed by rotating finned assembly at rear |
| GB2153982A (en) * | 1984-02-02 | 1985-08-29 | Dynamit Nobel Ag | Flight body |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2657703B1 (en) * | 1990-01-26 | 1992-04-10 | Thomson Brandt Armements | DEVICE FOR CONTROLLING THE ROLLING ATTITUDE OF A FIXTURE STABILIZED PROJECTILE. |
-
1971
- 1971-03-29 FR FR7110894A patent/FR2130968A5/fr not_active Expired
-
1972
- 1972-03-06 CH CH326272A patent/CH567708A5/xx not_active IP Right Cessation
- 1972-03-09 GB GB1113472A patent/GB1386350A/en not_active Expired
- 1972-03-13 ZA ZA721701A patent/ZA721701B/en unknown
- 1972-03-13 IL IL38967A patent/IL38967A/en unknown
- 1972-03-21 IT IT22141/72A patent/IT950409B/en active
- 1972-03-28 CA CA138,365A patent/CA956839A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2924217A1 (en) * | 1979-06-15 | 1980-12-18 | Rheinmetall Gmbh | Sub calibre shell for firing practice - has spin caused by released vaned adaptor opposed by rotating finned assembly at rear |
| GB2153982A (en) * | 1984-02-02 | 1985-08-29 | Dynamit Nobel Ag | Flight body |
Also Published As
| Publication number | Publication date |
|---|---|
| ZA721701B (en) | 1973-02-28 |
| CH567708A5 (en) | 1975-10-15 |
| CA956839A (en) | 1974-10-29 |
| IL38967A (en) | 1975-08-31 |
| IT950409B (en) | 1973-06-20 |
| IL38967A0 (en) | 1972-07-26 |
| FR2130968A5 (en) | 1972-11-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed [section 19, patents act 1949] | ||
| PCNP | Patent ceased through non-payment of renewal fee |