IL39475A - A unit in a carrier part in the form of a projectile,shell,etc.,comprised in and separable from the carrier part - Google Patents
A unit in a carrier part in the form of a projectile,shell,etc.,comprised in and separable from the carrier partInfo
- Publication number
- IL39475A IL39475A IL39475A IL3947572A IL39475A IL 39475 A IL39475 A IL 39475A IL 39475 A IL39475 A IL 39475A IL 3947572 A IL3947572 A IL 3947572A IL 39475 A IL39475 A IL 39475A
- Authority
- IL
- Israel
- Prior art keywords
- parts
- container
- tubular member
- unit
- flare
- Prior art date
Links
- 230000000875 corresponding effect Effects 0.000 claims 4
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
- F42B10/56—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding of parachute or paraglider type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/42—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of illuminating type, e.g. carrying flares
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Bag Frames (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE07576/71A SE368987B (enrdf_load_stackoverflow) | 1971-06-11 | 1971-06-11 |
Publications (2)
Publication Number | Publication Date |
---|---|
IL39475A0 IL39475A0 (en) | 1972-08-30 |
IL39475A true IL39475A (en) | 1976-01-30 |
Family
ID=20271751
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL39475A IL39475A (en) | 1971-06-11 | 1972-05-18 | A unit in a carrier part in the form of a projectile,shell,etc.,comprised in and separable from the carrier part |
Country Status (7)
Country | Link |
---|---|
US (1) | US3863569A (enrdf_load_stackoverflow) |
FR (1) | FR2141333A5 (enrdf_load_stackoverflow) |
GB (1) | GB1398774A (enrdf_load_stackoverflow) |
IL (1) | IL39475A (enrdf_load_stackoverflow) |
IT (1) | IT958151B (enrdf_load_stackoverflow) |
NL (1) | NL7207810A (enrdf_load_stackoverflow) |
SE (1) | SE368987B (enrdf_load_stackoverflow) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH621626A5 (enrdf_load_stackoverflow) * | 1977-09-02 | 1981-02-13 | Oerlikon Buehrle Ag | |
RU2144651C1 (ru) * | 1999-06-16 | 2000-01-20 | Государственное унитарное предприятие "Государственное научно-производственное предприятие "Сплав" | Боевая часть |
SE540780C2 (sv) * | 2016-04-06 | 2018-11-06 | Bae Systems Bofors Ab | Delningsbar granat med fallskärmsanordning |
SE540399C2 (sv) * | 2016-04-20 | 2018-09-11 | Bae Systems Bofors Ab | Stödanordning för delningsbar fallskärmsgranat |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1309982A (en) * | 1919-07-15 | Careieb-shell | ||
US2201482A (en) * | 1934-03-28 | 1940-05-21 | Jr Louis L Driggs | Flare casing and method of sealing |
US3143965A (en) * | 1959-11-06 | 1964-08-11 | Pointe Andre E La | Chaff dispenser |
US3374739A (en) * | 1966-03-16 | 1968-03-26 | Army Usa | Payload recovery system |
US3712232A (en) * | 1968-10-23 | 1973-01-23 | Us Navy | Variable delay fuse for aircraft parachute flare |
-
1971
- 1971-06-11 SE SE07576/71A patent/SE368987B/xx unknown
-
1972
- 1972-05-18 IL IL39475A patent/IL39475A/en unknown
- 1972-05-30 IT IT50609/72A patent/IT958151B/it active
- 1972-06-05 US US259985A patent/US3863569A/en not_active Expired - Lifetime
- 1972-06-08 GB GB2688672A patent/GB1398774A/en not_active Expired
- 1972-06-08 NL NL7207810A patent/NL7207810A/xx unknown
- 1972-06-09 FR FR7220835A patent/FR2141333A5/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
NL7207810A (enrdf_load_stackoverflow) | 1972-12-13 |
US3863569A (en) | 1975-02-04 |
GB1398774A (en) | 1975-06-25 |
IT958151B (it) | 1973-10-20 |
SE368987B (enrdf_load_stackoverflow) | 1974-07-29 |
FR2141333A5 (enrdf_load_stackoverflow) | 1973-01-19 |
DE2226717A1 (de) | 1972-12-14 |
IL39475A0 (en) | 1972-08-30 |
DE2226717B2 (de) | 1976-08-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA969117A (en) | Self-centering clutch release bearing assembly | |
GB1304671A (enrdf_load_stackoverflow) | ||
IL39475A (en) | A unit in a carrier part in the form of a projectile,shell,etc.,comprised in and separable from the carrier part | |
US3194161A (en) | Hand grenade | |
IL30095A0 (en) | Projectile having a useful charge which must be released at a point on the projectile trajectory | |
US3684214A (en) | Flying body having extensible fins | |
ATE85279T1 (de) | Reservefallschirm mit hilfs- oder pilotschirm. | |
GB851460A (en) | Improvements relating to the hollow-charge warheads of projectiles | |
US3366008A (en) | Lanyard | |
GB1355471A (en) | Carrier projectiles | |
US3135206A (en) | Fuze for projectiles | |
IL43946A (en) | Safety and arming device for fuses in launchable missiles | |
US1744233A (en) | Projectile for antiaircraft fire | |
EP0435919A1 (en) | SEPARATION DEVICE. | |
IL39530A (en) | Aerial flare with drogue parachute | |
US4926751A (en) | Arrangement for drawing a braking parachute out of an article of submunition | |
GB1174804A (en) | Improvements in Spinning Fuzes, in particular for Small Caliber Shells | |
STUFF | Head wave separation of a decelerating flying body during the transition from supersonic to subsonic velocity(Head wave separation from decelerating conical flying body during transition from supersonic to subsonic velocity) | |
GB1298652A (en) | Improvements relating to flare assemblies to be carried by projectiles | |
SU412410A1 (ru) | Устройство для быстрого разъединения узлов машин | |
ALFUTOV | Dependence of the value of the upper critical pressure of a cylindrical shell upon the boundary conditions for the tangential components of the displacements(Boundary conditions for tangential displacements effect upon value of critical pressure of closed circular cylindrical shell) | |
SU130797A1 (ru) | Водолазный скафандр | |
JPS6470299A (en) | Emergency parachute device | |
LUND | Observations on the development cycle for a navy air-to-air missile weapon system(Navy air to air missile weapon system development, examining test and evaluation stages) | |
COFER et al. | Experimental stress analysis of the attachment region of hemispherical shells with radially attached nozzles(Stress patterns for nozzle configurations for internal pressure, axial load on nozzle, pure bending moment on nozzle, shear load on nozzle, and pure torque on nozzle loadings) |