| astronautix.com | Rif-MA |
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| Rifma - Credit: © Mark Wade. 4,882 bytes. 18 x 81 pixels. |
Derived from SS-N-20 (RSM-52) SLBM. Air-launched from An-124. Ignition mass 79 tonnes.
LEO Payload: 1,500 kg. to: 200 km Orbit. Payload: 950 kg. to a: 700 km orbit trajectory.
![]() | ICBM-Derived LVs - The range of launch vehicles derived from decommissioned ballistic missiles offered for sale by Russia after the cold war. Credit: Mark Wade. 41,348 bytes. 640 x 444 pixels. |