| zpět | ruské mezikontinentální balistické rakety |
připravil Milan Božok
| NAVIGACE |
|
|
|
|
| Mod-1 | Mod-2 | Mod-3 | Mod-4 | |
DIA |
SS-11 | SS-11 | SS-11 | SS-11 |
| NATO | Sego | Sego | Sego | Sego |
| Označenie | UR-100/ UR-100M |
UR-100K | UR-100U | |
| OKB/Industry | 8K84 8K84UTTkh |
8K84K | 8K84UTTkh 8K84M 15A20U | |
| Dizajn | OKB-52 Chelomey |
OKB-52 Chelomey |
OKB-52 Chelomey |
OKB-52 Chelomey |
| Odsúhlasený | 3/30/1963 | |||
| Konštrukcia a testy | 1962-66 | 1969-1971 | 1971-1973 | 1971-1973 |
| Prvý test | 4/19/65 | 7/23/1969 | 2/2/71 & 9/2/69 | 6/16/71 |
| Dátum rozmiestnenia | 7/21/1967 | 12/28/72 | 9/26/1974 | [not deployed] |
| Typ hlavice | Single | Single | MRV | MRV |
| Hlavice | 1 | 1 | 3 | 6 |
| Mohutnosť (Mt) | 0.6 to 1.2 | 0.6 to 1.2 | 0.2 to 0.8 | |
| Užitočný náklad (t) | 0.76 - .08 | 0.9-1.2 | 1.208 | 1.2 |
| Dĺžka (m) | 16.925 | 18.9 - 19.0 | 18.9 | 19.1 - 19.8 |
| Dĺžka hlavice (m) | 16.45-16.69 | 16.5 | 17 | 17 |
| Priemer rakety (m) | 2 | 2. | 2 | 2 |
| Štartovacia váha (t) | 39.4 - 42.3 | 50.1 | 50.09 - 50.1 | 50.1 - 51.24 |
| Váha paliva (t) | 40.4? | 45.3 | 45.3 | 45.3 |
| Dosah (km) | 11,000-12,000 or 5,000 |
11,000-13,000 | 10,600-12,000 | 10,600-12,000 |
Copyright © All Rights Reserved