摘要 |
The missile is used in warfare technology for destroying armoured targets. It comprises a missile (1), ejection motor (2) and container (3). The missile (1) comprises a control compartment (7) with cross-contact (8), warhead (9) with a copper funnel (10), lens (11), briquettes of explosive (12 and 13) with a contact cone (15) connected to them, sustainer (16), control unit (17), coil (18) comprising a base (19) and fairing (20), interconnected in a fixed manner and enabling the winding of a conductor (21) of specified length. In the ejection motor (2), a charge of specific weight (4) is fitted, and the front and rear nozzle apertures have specified dimensions. 1 claim, 2 figures
|
申请人 |
"VMZ" EAD |
发明人 |
RACHEV, KHRISTO G.;KICHUKOV, NIKOLAJ T.;MANDADZHIEVA, DONKA N.;PUKOVA, VERA I.;BOCHKALIEVA, MITKA S.;RACHEVA, OLGA JU.;KARAMANSKA, STANKA P.;NESTOROVA, VELA K.;MILJANOVA, EKATERINA D.;PAVLOVA, MARIJA P.;KOEMDZHIEV, IVAN B.;ROGACHEV, TODOR P.;KRASTANOV, STANIMIR P.;KOLEV, GRIGOR M.;TSONKOVA, LJUDMILA V. |