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