公开(公告)号：WO2021257031A1

公开(公告)日：2021-12-23

申请号：PCT/TR2021/050574

申请日：2021-06-14

Applicant: ROKETSAN ROKET SANAYİİ TİCARET A. Ş.

Inventor： ATEŞOĞLU, Mustafa Özgür ,  MUHİDDİNOĞLU, Abdullah Alp ,  GÖRÜR, Bilge Kaan ,  ALTINTAŞ, Oğuz Han

IPC: F42B15/08 ,  F42B30/00 ,  F42B15/01 ,  F41G7/30 ,  G05D1/10 ,  F41G7/22

Abstract: The present invention relates to a distributed missile system having multiple miniature missile units (n) comprising the following; an elongated body (10) with a warhead (11); a drive motor (12) fixed to the body (10); a fin (14) that is provided in the body (10) and that rotates the body (10) towards a predetermined course during the cruise by being driven with the drive motor (12) and a controller (40) connected to the drive motor (12) to control the fin (14) position. The missile system comprises at least one relative awareness sensor (30) that scans the outer periphery of the body (10) by collecting 360° environmental awareness data (v) and transmits a signal to the controller (40).

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).