R-26 / "SS-8 SASIN"
Specifications | |||||
---|---|---|---|---|---|
DIA | Mistaken for SS-8/R-9,R-9A | ||||
NATO | Sasin mistaken for SS-8/R-9, R-9A | ||||
Bilateral | N/A | ||||
Service | Not deployed | ||||
OKB/Industry | R-26, 8K66 | ||||
Design Bureau | OKB-586 (Acad. M. K. Yangel) | ||||
Approved | 5/23/1960 | ||||
Years of R&D | |||||
Engineering and Testing | 1960-1961 | ||||
First Flight Test | Project canceled 07/09/1962 | ||||
IOC | Not operational | ||||
Deployment Date | Not deployed | ||||
Type of Warhead | Single | ||||
Warheads | 1 | ||||
Yield (Mt) | 5 | ||||
Payload (t) | 3-3.500 | ||||
Total length (m) | 24.38 | ||||
Total length w/o warhead (m) | 22 | ||||
Missile Diameter (m) | 2.75 | ||||
Launch Weight (t) | 85-87 | ||||
Fuel Weight (t) | |||||
Range (km) | 10,500-11,000-12,000 | ||||
CEP (m) (Russian Sources) | 1,500-2,000 | ||||
CEP (m) Western Sources) | ? |
Number of Stages | 2 |
Canister length (m) | N/A |
Canister length w/o front meters (m) |
N/A |
Canister diameter (m) | N/A |
Booster guidance system | Inertial |
1st stage | 2nd stage | |
---|---|---|
Length (m) | 11.4 | 10.05 |
Body diameter (m) | 2.75 | 2.4 |
Fueled weight (t) | ||
Dry weight (t) | ||
Engine Designation | RD-216 (11D614) | Z-RD-? |
Configuration | two engine cluster | 1 engine |
Design Bureau | Acad. V. P. Glushko OKB-456 | Yuzhnoy? |
Years of R & D | 1958-1960 | |
Propellants | Liquid Storable | Liquid Storable |
Fuel | UDMH | UDMH |
Oxidizer | AT=AK-27P,= Nitrogen tetroxide, N204 in N02 | AT=AK-27P,= Nitrogen tetroxide, N204 in N02 |
Burning time (sec.) | 160 | |
Thrust Sea Level/Vacuum (Tonnes) | 151.499/177.9115 | 43.65 vacuum |
Specific Impulse Sea Level/Vacuum (sec.) | 248/291.3 |
Basing Mode | Soft site and Silo |
Hardness | |
Launching Technique | Hot launch |
Deployed Boosters | 0 |
Test Boosters | |
Warheads Deployed | 0 |
Deployment Sites | |
Training Launchers | |
Space Booster Variant | N/A |
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