SE8105347L - AMMUNITION UNIT - Google Patents
AMMUNITION UNITInfo
- Publication number
- SE8105347L SE8105347L SE8105347A SE8105347A SE8105347L SE 8105347 L SE8105347 L SE 8105347L SE 8105347 A SE8105347 A SE 8105347A SE 8105347 A SE8105347 A SE 8105347A SE 8105347 L SE8105347 L SE 8105347L
- Authority
- SE
- Sweden
- Prior art keywords
- spike
- ammunition
- length
- unit
- ammunition unit
- 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
- F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
- F42B10/52—Nose cones
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Soil Working Implements (AREA)
Abstract
There is provided an ammunition unit, preferably for training purposes, intended to be fired from a gun barrel at supersonic speed. The ammunition unit comprises an intermediate body part (1) to which is connected a substantially cylindrical spike (2) as well as a finned tail section (3). The length (L1) and design of the spike and the design and connection of the tail section to the intermediate part are such that the ammunition unit, up to a predetermined firing distance, has substantially the same ballistic properties as the equivalent normal live ammunition but which has a significantly reduced maximal firing range as compared with such normal live ammunition. This is because a dead air stream zone is obtained around the spike at supersonic speeds, but at sub-sonic speeds the air stream follows the spike surface and results in a substantial braking force. The length L1 of the spike is 1.6-2.0 the diameter D of the body a truncated conical part 1a of the body has a length of 1-3% of the total length of the unit and a conical angle between 10 DEG and 20 DEG .
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8105347A SE444983B (en) | 1981-09-09 | 1981-09-09 | OVEN ENDAMAL EXTENSIBLE WINDOW STABILIZED AMMUNITION UNIT |
IL66658A IL66658A0 (en) | 1981-09-09 | 1982-08-27 | Ammunition unit,preferably for training purposes |
CH5153/82A CH658717A5 (en) | 1981-09-09 | 1982-08-30 | FLOOR, ESPECIALLY FOR EXERCISE PURPOSES. |
DK391882A DK153251C (en) | 1981-09-09 | 1982-09-01 | AMMUNITION UNIT, PRESENTLY FOR EXERCISE FORM |
DE19823233044 DE3233044A1 (en) | 1981-09-09 | 1982-09-06 | AMMUNITION UNIT, PREFERABLY FOR EXERCISE PURPOSES |
FR8215253A FR2512540B1 (en) | 1981-09-09 | 1982-09-08 | EXERCISE AMMUNITION FOR CANON |
NO823045A NO151640C (en) | 1981-09-09 | 1982-09-08 | AMMUNITION UNIT, EXERCISE FOR EXERCISE FORM |
GB08225595A GB2105445B (en) | 1981-09-09 | 1982-09-08 | Ammunition unit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8105347A SE444983B (en) | 1981-09-09 | 1981-09-09 | OVEN ENDAMAL EXTENSIBLE WINDOW STABILIZED AMMUNITION UNIT |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8105347L true SE8105347L (en) | 1983-03-10 |
SE444983B SE444983B (en) | 1986-05-20 |
Family
ID=20344518
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8105347A SE444983B (en) | 1981-09-09 | 1981-09-09 | OVEN ENDAMAL EXTENSIBLE WINDOW STABILIZED AMMUNITION UNIT |
Country Status (7)
Country | Link |
---|---|
CH (1) | CH658717A5 (en) |
DE (1) | DE3233044A1 (en) |
DK (1) | DK153251C (en) |
FR (1) | FR2512540B1 (en) |
GB (1) | GB2105445B (en) |
NO (1) | NO151640C (en) |
SE (1) | SE444983B (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3314750A1 (en) * | 1983-04-23 | 1984-10-25 | L'Etat Français représenté par le Délégué Général pour l'Armement, Paris | AGENT FOR IMPROVING THE RELEASE BEHAVIOR OF DRIVING CAGE SEGMENTS FROM A RIFLE BULLET FOR THE PIPE ARM |
DE3335997A1 (en) * | 1983-10-04 | 1985-04-11 | Rheinmetall GmbH, 4000 Düsseldorf | TRAINING FLOOR |
DE4132659A1 (en) * | 1991-10-01 | 1993-04-08 | Rheinmetall Gmbh | Vane-stabilised practice projectile for large calibre barrel weapon - has equal calibre central part supporting guide strip and connecting shaft part carrying vanes |
US5328130A (en) * | 1993-01-04 | 1994-07-12 | The United States Of America As Represented By The Secretary Of The Army | Stabilizer for a cannon projectile |
KR970705001A (en) * | 1995-06-07 | 1997-09-06 | 완다케이. 델슨-로우 | Gyroscope stabilized launch system for use in underwater objects |
DE102005039900A1 (en) * | 2005-08-24 | 2007-03-08 | Rheinmetall Waffe Munition Gmbh | Far-reaching full caliber bullet |
DE102013010356B3 (en) | 2013-06-21 | 2014-06-05 | Rheinmetall Waffe Munition Gmbh | Tail stabilized full caliber bullet |
CN110375594A (en) * | 2019-06-28 | 2019-10-25 | 南京理工大学 | A kind of supercavity long-tail projectile entering water suitable for low-angle |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE199366C (en) * | ||||
DE7732971U1 (en) * | 1978-05-24 | Rheinmetall Gmbh, 4000 Duesseldorf | Wing-stabilized training floor | |
DE267962C (en) * | ||||
GB103270A (en) * | 1915-11-16 | 1917-01-18 | Stanley Frederick Stokes | Improvements in Shells for Ordnance, Trench Guns and Mortars. |
FR1372604A (en) * | 1963-08-03 | 1964-09-18 | Flanged projectile in caliber | |
US3672304A (en) * | 1970-03-30 | 1972-06-27 | Lockheed Aircraft Corp | Special purpose firearms projectile |
US3786760A (en) * | 1972-06-01 | 1974-01-22 | Pacific Technica Corp | Rotating band for projectile |
GR65959B (en) * | 1977-10-26 | 1981-01-09 | Rheinmetall Gmbh | |
DE2759210A1 (en) * | 1977-12-31 | 1979-07-12 | Feistel Pyrotech Fab | Practice anti-tank missile - has tracer material between stabiliser fins and burning independently of temperature and pressure |
-
1981
- 1981-09-09 SE SE8105347A patent/SE444983B/en not_active IP Right Cessation
-
1982
- 1982-08-30 CH CH5153/82A patent/CH658717A5/en not_active IP Right Cessation
- 1982-09-01 DK DK391882A patent/DK153251C/en not_active IP Right Cessation
- 1982-09-06 DE DE19823233044 patent/DE3233044A1/en not_active Withdrawn
- 1982-09-08 NO NO823045A patent/NO151640C/en unknown
- 1982-09-08 FR FR8215253A patent/FR2512540B1/en not_active Expired
- 1982-09-08 GB GB08225595A patent/GB2105445B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB2105445A (en) | 1983-03-23 |
SE444983B (en) | 1986-05-20 |
DK153251B (en) | 1988-06-27 |
NO151640C (en) | 1985-05-08 |
GB2105445B (en) | 1985-05-15 |
DK153251C (en) | 1988-12-05 |
FR2512540B1 (en) | 1987-05-29 |
DK391882A (en) | 1983-03-10 |
DE3233044A1 (en) | 1983-03-24 |
NO151640B (en) | 1985-01-28 |
CH658717A5 (en) | 1986-11-28 |
FR2512540A1 (en) | 1983-03-11 |
NO823045L (en) | 1983-03-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |
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