Active semi-active homing head 9B-1103M-200PA is designed for installation on air-to-air missiles designed to destroy aircraft, helicopters (including hovercrafts), cruise and anti-location missiles.
The potential carriers of the 9B-1103M-200PA are medium-range aircraft rockets of the RVV-SD type and long-range aircraft rockets of the RVV-AE-PD type.
The developer is the Agat Moscow Research Institute.
GSN 9B-1103M-200PA was demonstrated at the MAKS-2011 aerospace exhibition, the International Forum "Technologies in Mechanical Engineering 2014".
GSN 9B-1103M-200PA - combined antenna. In the active mode the homing head works in Ku-band, using waveguide and slot antenna, in semi-active mode the antenna grating of 12-16 dipoles installed on the front surface of the antenna is used (see photo).
The composition of the CNS:
- managed coordinator with antenna
- transmitting channel
- receiving channel
- programmable on-board computer system
ARGS 9B-1103M-200PA provides:
- searching, capturing and escorting air targets;
- receiving and decoding radiocorrection signals;
- formation and transmission of signals over a digital communication line for missile control ;
Modes of operation:
- Fully autonomous (active) mode by pre-targeting without radar support in flight (the "let-forget" mode);
- inertial guidance mode with radiocorrection;
- reprogramming mode.
|Target acquisition range with (EEP=3 m2), km:
- inertial-semi-active mode
- active mode
80 – 100
|Speed range of targets||0,1 – 5М|
- minimum flight height, m
-effective reflective surface, m2
50 – 1200
|Ready time, s:
- not pre-turned on
- upon initial activation
5 – 8
|Operation range of the active channel||Ku|
|Operation range of the semi-active channel||Ku|
-length (without fairing)