Sheldon / Dod | Name | Article | Designation | Comment |
A / SL1 | R7 | 8K71 | ||
A / SL1 | Sputnik | ? | 8K71PS | for the first 2 Sputniks |
A / SL2 | Sputnik | ? | 8A91 | for Sputnik (3) failure and Sputnik-3 |
A1 / SL3 | Vostok L (Luna?) | ? | 8Kxx | for early Lunas and the first Korabl-Sputnik |
A1 / SL3 | Vostok K | ? | 8KxxK | for Korabl-Sputniks and Vostoks |
A1 / SL3 | Vostok | ? | 8A92 | for Cosmos series (Zenit) spysats and early Meteors |
A1 / SL3 | Vostok M | ? | 8A92M | for sunsynchronous missions |
A2 / SL4 | Voskhod | ? | 11A57 ? | for the first missons and for Voskhod |
A2 / SL4 | Soyuz | ? | 11A511 | for Soyuz capsules |
A2 / SL4 | Soyuz M | ? | 11A511M | |
A2 / SL4 | Soyuz L | ? | 11A511L | to lift Cosmos 398 class Lunar lander tests into LEO |
A2 / SL4 | Soyuz U | ? | 11A511U | the current model for unmanned missions |
A2 / SL4 | Soyuz U2 | ? | 11A511U2 | the current version for manned missions (and possibly for Kuban type spysats) |
A2e / SL6 | Molniya | ? | 8K78 | was used only until 1966 |
A2e / SL6 | Molniya M | ? | 8K78M | the current model |
Ae / SL5 | Sputnik-Polyot | ? | 11A?? | Polyot launch vehicle |
A1m / SL10 | ? | ? | 11A510 | Cosmos 125 / 102 launch vehicle |
B1 / SL7 | Cosmos 1 | ? | 63S1 | difference unknown |
B1 / SL7 | Cosmos B | ? | 11K63 | difference unknown |
C1 / SL8 | ? | ? | 65S1 | Tyuratam launch |
C1 / SL8 | Cosmos 3 | ? | 11K65 | Tyuratam launch |
C1 / SL8 | Cosmos 3M | ? | 11K65M | Kapustin Yar and Plesetsk launch |
D / SL9 | Proton | UR500 | 8K82 | two stage test version |
D1 / SL13 | Proton K | UR500K | 8K82K | three stage version for LEO |
D1e / SL12 | Proton K Block D | UR-500K Block D | 11S824 | for early interplanetary probes |
D1e / SL12 | Proton K Block DM | UR-500K Block DM | 11S86 | for early GEO missions |
D1e / SL12 | Proton K Block DM2 | UR-500K Block DM2 | 11S861 | uprated version of Block DM |
D1e / SL12 | Proton K Block DM2M | UR-500K Block DM2M | 11S861-01 | lightwight version of Block DM2 for higher payloads |
G1e / SL15 | N1 / L3 | ? | ||
G1e / SL15 | N1 / L3 (7L) | L | N-1 L3 (7L) had different boattail | |
F1r / SL11 | R36-0 | 8K69 | for FOBS | |
F1m / SL11 | Cyclone M (or 2) | ? | 11K69 | |
F2 / SL14 | Cyclone 3 | ? | 11K68 | |
J1 / SL16 | Zenit 2 | ? | 11K77 | |
K1 / SL17 | Energiya | ? | ? | |
Dnepr | R36-M2 | 15A18M |
RS-20
/ SS-18 150 missiles in reserve before first space launch Operated by the Russian-Ukrainian Cosmotras company fired from a silo launch pad | |
Strela |
RS-18 first launch in late 2002 from Tyuratam Can orbit 600 to 1700 kg to 300 to 1500 km orbit. Should cost $9 million for commercial launches. |