Orbital launch vehicle
Volna
Space launch vehicle Volna is a converted Submarine-launched ballistic missile used for launching satellites into orbit. It is based on the R-29R designed by State Rocket Center Makayev and related to the Shtil' Launch Vehicle . The Volna is a 3-stage launch vehicle that uses liquid propellant. The warhead section is used for the payloads that can be either put into orbit with the help of an additional boost engine or travel along a sub-orbital trajectory to be recovered at the landing site. Volna can be launched from Delta III-class submarine or from land based facilities.
Volna is built by Makeyev Rocket Design Bureau of Russia. It first flew on 21 June 2005 and last flew on 21 June 2005.
Flight record
Payload
| Low Earth orbit | 120kg |
|---|
Vehicle
| Stages | 3 |
|---|---|
| Length | 14.1m |
| Diameter | 1.9m |
| Launch mass | 35t |
| Liftoff thrust | 682kN |
| Maiden flight | 1975-01-01 |
| Reusable | No |
Pads used
Orbits delivered
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| 2005-06-21 | Volna | Cosmos-1 | Borisoglebsk (K-496) | Low Earth Orbit | Failure |
Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.
Further reading: Wikipedia
Fewer than three recorded flights, so this page is marked noindex. It is here for completeness, not for search.