ES2920528T3 - Procedimiento para lanzar un misil guiado desde una plataforma portadora y misil guiado - Google Patents

Procedimiento para lanzar un misil guiado desde una plataforma portadora y misil guiado Download PDF

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Publication number
ES2920528T3
ES2920528T3 ES21162240T ES21162240T ES2920528T3 ES 2920528 T3 ES2920528 T3 ES 2920528T3 ES 21162240 T ES21162240 T ES 21162240T ES 21162240 T ES21162240 T ES 21162240T ES 2920528 T3 ES2920528 T3 ES 2920528T3
Authority
ES
Spain
Prior art keywords
guided missile
carrier platform
flight
rudder elements
rudder
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.)
Active
Application number
ES21162240T
Other languages
English (en)
Spanish (es)
Inventor
Peter Gerd Fisch
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Diehl Defence GmbH and Co KG
Original Assignee
Diehl Defence GmbH and Co KG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Diehl Defence GmbH and Co KG filed Critical Diehl Defence GmbH and Co KG
Application granted granted Critical
Publication of ES2920528T3 publication Critical patent/ES2920528T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

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)
ES21162240T 2020-03-14 2021-03-12 Procedimiento para lanzar un misil guiado desde una plataforma portadora y misil guiado Active ES2920528T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102020001703.7A DE102020001703A1 (de) 2020-03-14 2020-03-14 Flugkörper, Flugzeug mit dem Flugkörper sowie Verfahren zum Abwerfen eines Flugkörpers aus einem Flugzeug

Publications (1)

Publication Number Publication Date
ES2920528T3 true ES2920528T3 (es) 2022-08-05

Family

ID=74873538

Family Applications (1)

Application Number Title Priority Date Filing Date
ES21162240T Active ES2920528T3 (es) 2020-03-14 2021-03-12 Procedimiento para lanzar un misil guiado desde una plataforma portadora y misil guiado

Country Status (3)

Country Link
EP (1) EP3882564B1 (de)
DE (1) DE102020001703A1 (de)
ES (1) ES2920528T3 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115164653B (zh) * 2022-06-30 2023-12-05 河北汉光重工有限责任公司 一种舵片零位组合式调试装置及调试方法
CN117048849B (zh) * 2023-10-13 2024-01-23 四川腾盾科技有限公司 一种拉桨式无人机投送翼挂吊舱的飞行测试方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3355130A (en) 1965-12-10 1967-11-28 Vernon C Dell Anti-squeeze mode control surface mechanism
US4072107A (en) 1967-06-07 1978-02-07 The United States Of America As Represented By The Secretary Of The Army Missile control means
US4044970A (en) * 1975-08-08 1977-08-30 General Dynamics Corporation Integrated thrust vector aerodynamic control surface
US5048773A (en) 1990-06-08 1991-09-17 The United States Of America As Represented By The Secretary Of The Army Curved grid fin
US9587922B2 (en) * 2013-04-12 2017-03-07 Raytheon Company Attack capability enhancing ballistic sabot
US10539403B2 (en) * 2017-06-09 2020-01-21 Kaman Precision Products, Inc. Laser guided bomb with proximity sensor
KR102136266B1 (ko) 2019-01-14 2020-07-21 국방과학연구소 유도탄 비행속도 감소를 위한 무기동 제동날개변위 명령 산출 및 적용 방법

Also Published As

Publication number Publication date
DE102020001703A1 (de) 2021-09-16
EP3882564B1 (de) 2022-05-11
EP3882564A1 (de) 2021-09-22

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