FIELD: rocketry. SUBSTANCE: anti-aircraft target missile has a propulsion system with a fin and a nose section with a fairing. The nose section is made as a radioparent shell of composite material accommodating corner reflectors of SHF-energy. The reflectors are made in the form of mutually perpendicular metal plates fastened to one another. Connected from the front to the nose section by means of fairing is a steel hollow end-piece accommodating the flares, and the body has through diameter slots. The total area of the end-piece slots exceeds or equals the sectional area of the flares. EFFECT: simulation of characteristic of re-emission of SHF-energy by missile means of air attack during testings of anti-aircraft missile systems. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
ANTI-AIRCRAFT TARGET MISSILE | 2000 |
|
RU2196953C2 |
ANTI-AIRCRAFT TARGET MISSILE | 2002 |
|
RU2222767C1 |
ANTI-AIRCRAFT TARGET MISSILE | 2006 |
|
RU2317511C1 |
ANTI-AIRCRAFT MISSILE-TARGET | 2005 |
|
RU2288432C1 |
AIR DEFENCE MISSILE TARGET | 2006 |
|
RU2326339C1 |
TARGET ROCKET | 2010 |
|
RU2415372C1 |
AERIAL TARGET SIMULATOR | 2020 |
|
RU2769455C1 |
AIR TARGET SIMULATOR | 2017 |
|
RU2651457C1 |
ANTIAIRCRAFT GUIDED MISSILE | 1998 |
|
RU2133446C1 |
GUIDED ANTI-AIRCRAFT MISSILE | 2000 |
|
RU2167390C1 |
Authors
Dates
1999-08-27—Published
1998-06-09—Filed