| 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 |