| Technical data |
| Type |
RSS (S-30) |
| Function |
Guided cruise missile |
| Year |
1953
|
| Crew |
- |
| Engine |
? |
| Length |
?m |
| Height |
?m |
| Wingspan |
?m |
| Wing area |
?m2 |
| Loaded weight |
?kg |
| Speed |
?km/h |
| Range |
?km |
| Payload |
| Fuel |
?kg |
| Warhead |
Nuclear |
RSS (S-30) project by N.V.Tsybin
In 1953 N.V.Tsybin started working on a project of heavy guided missile RSS (S-30) within S.P.Korolev's OKB-1. Missile was designed for strategic bombers A-57 and M-50 (under development by R.L.Bartini and V.M.Myasichev) or by specially modified Tu-95-S30. Flight control and aiming of the RSS had to be performed by operator(s) at the carrier aircraft (sheep-and-Shepard scheme).
Soon it became clear that range of reliable aiming does not allow the carrier to evade 'potential enemy' anti-aircraft defenses. At the time self-guided systems were introduced (including ones using stars), and project was cancelled. Team switched to a single-seat strategic supersonic bomber (project RS).
| Predecessors |
Modifications |
| - |
RS
|
| References |
Links |
|
|
- P.V.Tsibin at 'True Supersonics'
- R-020/RSR/NM-1 Page
- 'Ahead of Time'
|