he analysis of methods of construction and application of modern anti-radar
missiles (ARM) is carried out. The analysis allowed us to identify the most distinctive features
of ARM such as: high flight speed (600-1200 m/s), limited launch range, different flight paths
and it is oriented towards the attacked radar, small effective distribution surface (ESR), due to
a sharp increase in the weight and size characteristics of the homing head of the homing head
outside the frequency range (from 0.5 to 40 GHz), radio electronic means of the ARM are not
created, the large range and high speed of tuning the operating frequency of the receiver of
the homing head make it inefficient to use frequency jumps in electronic means, modern ARM
has an autonomous inertial guidance system, corrected from the NAVSTAR (Navigation
Satellites providing Time And Range) satellite radio navigation system via a GPS (Global
positioning system) receiver which are physical prerequisites for their effective selection. The
findings obtained during the analysis will be used in the development of a device for selecting
an anti-radar missile aimed at a surveillance radar, as well as for taking effective measures to
protect electronic equipment from them.
he analysis of methods of construction and application of modern anti-radar
missiles (ARM) is carried out. The analysis allowed us to identify the most distinctive features
of ARM such as: high flight speed (600-1200 m/s), limited launch range, different flight paths
and it is oriented towards the attacked radar, small effective distribution surface (ESR), due to
a sharp increase in the weight and size characteristics of the homing head of the homing head
outside the frequency range (from 0.5 to 40 GHz), radio electronic means of the ARM are not
created, the large range and high speed of tuning the operating frequency of the receiver of
the homing head make it inefficient to use frequency jumps in electronic means, modern ARM
has an autonomous inertial guidance system, corrected from the NAVSTAR (Navigation
Satellites providing Time And Range) satellite radio navigation system via a GPS (Global
positioning system) receiver which are physical prerequisites for their effective selection. The
findings obtained during the analysis will be used in the development of a device for selecting
an anti-radar missile aimed at a surveillance radar, as well as for taking effective measures to
protect electronic equipment from them.
| № | Author name | position | Name of organisation |
|---|---|---|---|
| 1 | A S.S. | teacher | Radar and receiving and transmitting devices educational institution of the Military Academy of the Republic of Belarus |
| 2 | P A.K. | teacher | Institute of applied Physics of the National Academy of Sciences of Belarus |
| 3 | B M.M. | teacher | Higher military aviation school |
| 4 | G S.T. | teacher | Higher military aviation school |
| № | Name of reference |
|---|---|
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| 12 | B.M. Mukhammedov. Analysis of existing radar protection systems from anti-radar missiles and substantiation of the appearance of radar protection from ARM using the RSP-10MA radar landing system as an example. “Bulletin of the Academy of the Armed Forces of the Republic of Uzbekistan”. 2021. 82. |
| 13 | B.P. Boysunov., H.A. Usmanova., N.E. Sheina. Reliability and quality of radioelectronic equipment. “Science magazine. technic stars, 1-2 special number”, 2019. 74. |
| 14 | P.A. Khmarski., D.S. Shilov., B.M. Mukhammedov. A device for detecting the trajectory of an anti-radar missile aimed at a control radar. “X International Scientific and Practical Conference Military Academy of the Republic of Belarus”, 2020 |
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