JPS5291599A - Spike-nose for launching vehicle - Google Patents
Spike-nose for launching vehicleInfo
- Publication number
- JPS5291599A JPS5291599A JP717976A JP717976A JPS5291599A JP S5291599 A JPS5291599 A JP S5291599A JP 717976 A JP717976 A JP 717976A JP 717976 A JP717976 A JP 717976A JP S5291599 A JPS5291599 A JP S5291599A
- Authority
- JP
- Japan
- Prior art keywords
- spike
- nose
- launching vehicle
- launching
- vehicle
- 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.)
- Pending
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
-
- 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
- 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
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
- F42B12/105—Protruding target distance or stand-off members therefor, e.g. slidably mounted
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
Abstract
PURPOSE:To improve a form of spike-nose for a launching vihicle and elevate a stability of the flying body.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP717976A JPS5291599A (en) | 1976-01-27 | 1976-01-27 | Spike-nose for launching vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP717976A JPS5291599A (en) | 1976-01-27 | 1976-01-27 | Spike-nose for launching vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5291599A true JPS5291599A (en) | 1977-08-02 |
Family
ID=11658839
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP717976A Pending JPS5291599A (en) | 1976-01-27 | 1976-01-27 | Spike-nose for launching vehicle |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5291599A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2627273A1 (en) * | 1988-02-17 | 1989-08-18 | Saint Louis Inst | FLYING ENGINE WITH GAS EJECTION NOZZLES |
EP1862758A2 (en) | 2006-05-31 | 2007-12-05 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Missile for the supersonic range |
RU2825777C2 (en) * | 2023-02-22 | 2024-08-30 | Российская Федерация, от имени которой выступает Министерство обороны РФ | Reactive assault grenade warhead |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3713607A (en) * | 1968-08-15 | 1973-01-30 | Us Navy | Load reducing spike for supersonic missiles |
-
1976
- 1976-01-27 JP JP717976A patent/JPS5291599A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3713607A (en) * | 1968-08-15 | 1973-01-30 | Us Navy | Load reducing spike for supersonic missiles |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2627273A1 (en) * | 1988-02-17 | 1989-08-18 | Saint Louis Inst | FLYING ENGINE WITH GAS EJECTION NOZZLES |
EP1862758A2 (en) | 2006-05-31 | 2007-12-05 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Missile for the supersonic range |
EP1862758A3 (en) * | 2006-05-31 | 2008-08-13 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Missile for the supersonic range |
RU2825777C2 (en) * | 2023-02-22 | 2024-08-30 | Российская Федерация, от имени которой выступает Министерство обороны РФ | Reactive assault grenade warhead |
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