D-6 Specifications
| VARIANT "B" | VARIANT "C" | |
|---|---|---|
| Developer | CDB-7 (KB Arsenal) | CDB-7 (KB Arsenal) |
| Chief Designer | P.A.Tyurin | P.A.Tyurin |
| manufacturer | plant No. 7 | plant No. 7 |
| type | strategic missile complex with solid propellant ballistic missile to shoot at stationary onshore targets | |
| Ships-carriers | PL etc. 629 658 D6, D6 | 629 D6, D6, 658 667 (option) |
| status of work | 1958-1960 | 1958-1961 |
| Performance | ||
| Range of fire, km: | ||
| project of 1958 | more than 800 | more than 800 |
| prospective (1958 year) | 2500 | 2500 |
| project 1960 year | 1100 | |
| prospective (1960 onwards) | 1500 | |
| Maximum deviation from target to maximum range | ... | |
| by range (1958 year) | +4 | +4 |
| lateral deviation (1958 year) | +4 | +4 |
| by range (1960 year) | +5 | |
| lateral deviation (1960 year) | +4 | |
| Payload | ||
| Head part: | ... | |
| Developer | NII-1011 MSM | |
| monoblock type | nuclear (Special) type "49" | nuclear (Special) type "49" |
| weight, kg | 500-1200 | 500-1200 |
| weight charge | 850 kg | |
| power charge, Mt | 0.3 -1 | 0.3 -1 |
| type of fuse | contact and uncontact sensors | |
| Developer of uncontact sensors | NII-137 GKOT | |
| Developer of contact sensors | SKB 885-GKRJe | |
| Control system | autonomous inertial | autonomous inertial |
| Developer | NII-592 | NII-592 |
| Designer | N.A.Semihatov | N.A.Semihatov |
| Developer of gyroscopic devices | NII-49 | NII-49 |
| Controls | swivelling nozzles | swivelling nozzles |
| Configuration | ||
| Start type | dry underwater from the tube by starter motors | |
| Start depth, | m 30-50 | ... |
| project of 1958 | 30-50 | |
| project of 1960 | 40-50 | |
| Number of steps | 2 | 2 |
| Dimensions, m: | ||
| full length | 14.4 -15.0 | -15.0 14.15 |
| Max. case diameter | 1.85 | 1.8 |
| Starting weight, t | 21-22.5 | 21.5 - 26 |
| Fuel | ballistic powder | composite solid |
| first stage | ||
| Mill-type | IR-190 | IR-194 |
| Curb weight is steps t | 12.2 | 14.7 |
| Fuel weight, t | 4 x 2.5 | 12.2 |
| Max. case diameter | 1.85 m | 1.8 m |
| Propulsion | four solid rocket motors in the same block | single chamber |
| Developer | TSKB-7 | TSKB-7 |
| fuel type | ballistitnoe "-b" | composite "Nylon" |
| fuel developer | NII-125 | GIPH |
| HL. Designer | B.p. Zhukov | Vs Shpak |
| specific impulse | on the ground, 210-220 | |
| Chamber pressure | combustion, kg/cm2 30-40 | |
| second stage | ||
| Mill-type | IR-191 | IR-189 |
| Curb weight t | 6.6 | 5.85 |
| Dimensions, m: | ||
| Max. case diameter | 1.7 | 1.8 m |
| Propulsion | four solid rocket motors in the same block | SPRE single Chamber |
| Developer | TSKB-7 | TSKB-7 |
| fuel type | ballistitnoe "-b" | composite "Nylon" |
| fuel developer | NII-125 | GIPH |
| HL. Designer | B.p. Zhukov | Vs Shpak |
| fuel weight, t | 4 x 1.3 | 4.7 |
| single pulse | ||
| on Earth | 220 | |
| Chamber pressure | combustion, kg/cm2 30-40 | |
| Launch ["start"] | ||
| Starter engines: | ||
| Developer works | no. 81 GKAT | KB-2 factory No. 81 GKAT and NII-125 GKOT |
| Type powder | DWP-78 | Fuel-Solid "Nylon-B" |
| Number | 6 engines (8) | 6 engines (8) |
| LAUNCHER: | ||
| Developer | CDB-34 | ... |
| Silo type | SM-93 | |
| Dimensions, m: | ||
| length | 16.0 | 16.0 |
| diameter | 2-2.15 | 2.15 |
| The number of rockets on PU | 1 | 1 |
| SHIP CONTROL SYSTEM: | ... | |
| Developer | NII-49 | NII-49 |
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