公开(公告)号：WO2021251932A1

公开(公告)日：2021-12-16

申请号：PCT/TR2021/050545

申请日：2021-06-07

Applicant: ROKETSAN ROKET SANAYİİ TİCARET A. Ş.

Inventor： ATEŞOĞLU, Mustafa Özgür ,  YÜKSEL, Muhammed ,  TEKEREK, Ali Şimşek ,  SEÇKİN UZEL, Öznur Cansu ,  MUHİDDİNOĞLU, Abdullah Alp

IPC: F41G7/22 ,  F42B15/01

Abstract: The present invention relates to a laser-guided miniature missile system comprising a launch station (70); and a miniature missile (30) that is provided in said launch station (70), that has an elongated body (32) configured such that it may be launched from a canister (10) or a launch pod (20). The inventive miniature missile system comprises; a remote control station (80) that is connected such that it communicates by means of an RF receiver/transmitter (74) of the launch station (70) accommodated on a mobile vehicle (1) and an opposite RF receiver/transmitter (82); a central controller (72) that triggers a canister (10) or a launch pod (20) such that they launch the miniature missile (30) by means of a pod control member (76) driven by determining a launch command transmitted from the control station (80) to the launch station (70); and a flight controller (38) to the which the central controller (72) is connected such that said central controller (72) ensures signal transmission in a storage mode and that is mounted on the body (32) that activates a flight motor (38) at a predetermined flight motor activation time (t2) by being configured such that it can interrupt the signal communication with the central controller (72) subsequent to a launching moment (t0).

公开(公告)号：WO2021251933A1

公开(公告)日：2021-12-16

申请号：PCT/TR2021/050546

申请日：2021-06-07

Applicant: ROKETSAN ROKET SANAYİİ TİCARET A. Ş.

Inventor： ATEŞOĞLU, Mustafa Özgür ,  YÜKSEL, Muhammed ,  MUHİDDİNOĞLU, Abdullah Alp ,  TEKEREK, Ali Şimşek ,  SEÇKİN UZEL, Öznur Cansu ,  YAYLA, Koray

IPC: F41G7/22 ,  F42B15/01

Abstract: The present invention relates to a miniature missile system having a hollow grenade launcher barrel (10) equipped with a trigger (2) and also a miniature missile (30) with a body (32) positioned on the barrel (10). Said missile system comprises a launching capsule (20) with a powder chamber (22) adjusted, such that it is provided at the rear portion (14) of the barrel (10) and creates a launching pressure area (23) allowing for raising the body (34) up to an effective flight height (h) from the barrel (10) in a ground level at the rear portion of the body (32), when activated by the trigger (2). Said miniature missile (30) comprises a flight controller (38) configured to actuate a flight motor (34) at the rear portion of the body (34), when reached up the flight height (h).