FR2724221A1 - Projectile comprenant une charge utile destinee a etre mise en oeuvre a altitude controlee - Google Patents
Projectile comprenant une charge utile destinee a etre mise en oeuvre a altitude controlee Download PDFInfo
- Publication number
- FR2724221A1 FR2724221A1 FR9410560A FR9410560A FR2724221A1 FR 2724221 A1 FR2724221 A1 FR 2724221A1 FR 9410560 A FR9410560 A FR 9410560A FR 9410560 A FR9410560 A FR 9410560A FR 2724221 A1 FR2724221 A1 FR 2724221A1
- Authority
- FR
- France
- Prior art keywords
- parachute
- payload
- projectile
- projectile according
- deployable
- 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.)
- Granted
Links
- 230000000087 stabilizing effect Effects 0.000 claims description 25
- 239000003380 propellant Substances 0.000 claims description 6
- 230000001174 ascending effect Effects 0.000 claims description 2
- 230000003019 stabilising effect Effects 0.000 abstract 1
- 230000006641 stabilisation Effects 0.000 description 5
- 238000011105 stabilization Methods 0.000 description 5
- 239000003381 stabilizer Substances 0.000 description 3
- 239000007789 gas Substances 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9410560A FR2724221A1 (fr) | 1994-09-02 | 1994-09-02 | Projectile comprenant une charge utile destinee a etre mise en oeuvre a altitude controlee |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9410560A FR2724221A1 (fr) | 1994-09-02 | 1994-09-02 | Projectile comprenant une charge utile destinee a etre mise en oeuvre a altitude controlee |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2724221A1 true FR2724221A1 (fr) | 1996-03-08 |
FR2724221B1 FR2724221B1 (enrdf_load_stackoverflow) | 1997-02-21 |
Family
ID=9466657
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9410560A Granted FR2724221A1 (fr) | 1994-09-02 | 1994-09-02 | Projectile comprenant une charge utile destinee a etre mise en oeuvre a altitude controlee |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2724221A1 (enrdf_load_stackoverflow) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2249784C2 (ru) * | 2003-03-03 | 2005-04-10 | Акционерное общество открытого типа "Институт прикладной физики" | Турбореактивный снаряд радиолокационных помех |
RU2296944C1 (ru) * | 2005-08-01 | 2007-04-10 | Открытое акционерное общество "Институт прикладной физики" | Снаряд-постановщик ложной радиолокационной цели |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3055300A (en) * | 1956-04-06 | 1962-09-25 | Stoehr Donald | Rocket flare head |
US3730099A (en) * | 1970-12-17 | 1973-05-01 | Us Navy | Controlled descent system |
US3834312A (en) * | 1973-03-14 | 1974-09-10 | Bofors Ab | Parachute-borne flare assemblage |
DE2611206A1 (de) * | 1976-03-17 | 1977-09-29 | Diehl Fa | Leuchtwurfkoerper |
GB2003588A (en) * | 1977-09-02 | 1979-03-14 | Oerlikon Buehrle Ag | Projectile |
US4632010A (en) * | 1985-04-01 | 1986-12-30 | The United States Of America As Represented By The Secretary Of The Navy | AIRBOC chaff deployment system |
FR2590664A1 (fr) * | 1977-03-28 | 1987-05-29 | France Etat Armement | Tete militaire |
-
1994
- 1994-09-02 FR FR9410560A patent/FR2724221A1/fr active Granted
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3055300A (en) * | 1956-04-06 | 1962-09-25 | Stoehr Donald | Rocket flare head |
US3730099A (en) * | 1970-12-17 | 1973-05-01 | Us Navy | Controlled descent system |
US3834312A (en) * | 1973-03-14 | 1974-09-10 | Bofors Ab | Parachute-borne flare assemblage |
DE2611206A1 (de) * | 1976-03-17 | 1977-09-29 | Diehl Fa | Leuchtwurfkoerper |
FR2590664A1 (fr) * | 1977-03-28 | 1987-05-29 | France Etat Armement | Tete militaire |
GB2003588A (en) * | 1977-09-02 | 1979-03-14 | Oerlikon Buehrle Ag | Projectile |
US4632010A (en) * | 1985-04-01 | 1986-12-30 | The United States Of America As Represented By The Secretary Of The Navy | AIRBOC chaff deployment system |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2249784C2 (ru) * | 2003-03-03 | 2005-04-10 | Акционерное общество открытого типа "Институт прикладной физики" | Турбореактивный снаряд радиолокационных помех |
RU2422759C2 (ru) * | 2003-03-03 | 2011-06-27 | Анатолий Яковлевич Скударнов | Турбореактивный снаряд радиолокационных помех |
RU2296944C1 (ru) * | 2005-08-01 | 2007-04-10 | Открытое акционерное общество "Институт прикладной физики" | Снаряд-постановщик ложной радиолокационной цели |
Also Published As
Publication number | Publication date |
---|---|
FR2724221B1 (enrdf_load_stackoverflow) | 1997-02-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2654505A1 (fr) | Sous-munition de projectile d'artillerie. | |
EP0318359B1 (fr) | Dispositif de déploiement d'une ailette de projectile | |
WO2011080410A1 (fr) | Systeme d'emport et de largage de charge pour avion de transport | |
FR2511340A1 (fr) | Systeme de recuperation et/ou de lancement d'un aeronef | |
FR2664233A1 (fr) | Dispositif de securite assurant la survie du personnel naviguant a bord d'aeronefs. | |
CH660157A5 (fr) | Installation d'alarme d'une vitesse de descente excessive pour avion a aile tournante. | |
FR2595811A1 (fr) | Projectile porteur pour sous-munitions | |
FR3088894A1 (fr) | Système de récupération d’un engin spatial en mer, procédé de récupération et utilisation associés à celui-ci | |
WO1991019645A1 (fr) | Dispositif articule pour vehicule spatial, notamment pour l'obturation temporaire de l'orifice d'entree d'un instrument optique spatial | |
EP4251517A1 (fr) | Systeme de transport spatial reutilisable | |
FR2724221A1 (fr) | Projectile comprenant une charge utile destinee a etre mise en oeuvre a altitude controlee | |
FR2629908A1 (fr) | Dispositif de freinage aerodynamique d'un corps | |
FR2664375A1 (fr) | Mine comprenant un dispositif de mise en position. | |
EP2354000B1 (fr) | Système d'emport de charge pour avion de transport | |
EP0546888A1 (fr) | Obus dont le culot fait office de pot de parachute d'une sous-munition | |
CA1314531C (fr) | Corps largable muni de moyens de freinage aerodynamique | |
FR2728229A1 (fr) | Bouclier de freinage pour engin spatial et satellite ainsi equipe | |
FR2619441A1 (fr) | Bombe antipiste a haute perforation | |
WO2018059932A1 (fr) | Procédé de guidage d'une cabine d'ascenseur de simulation de gravité réduite par rapport à la gravité terrestre | |
EP0047211A1 (fr) | Procédé de changement d'orbite d'un satellite, notamment d'injection en orbite géostationnaire et satellite mettant en oeuvre ledit procédé | |
FR2769083A1 (fr) | Procede de guidage d'un missile et missile pour la mise en oeuvre du procede | |
EP0434549B1 (fr) | Système de retenue de sous-munitions embarquées dans un vecteur | |
FR2724222A1 (fr) | Engin volant, notamment missile ou roquette, comprenant deux parties separables sur trajectoire | |
EP1544101A1 (fr) | Procédé pour améliorer la manoeuvrabilité d'un aéronef lors d'une ressource | |
EP0370855A1 (fr) | Dispositif de verrouillage et de déverrouillage de deux éléments d'un projectile, notamment d'un pot de parachute |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20110531 |