BUILDER(S) Makeyev OKB, Russia (design bureau) USERS/PLATFORMS

BUILDER(S)

USERS/PLATFORMS

CHARACTERISTICS

Missile 41,667 lb (18,900 kg)

Throwweight 1,500 lb ( 680 kg)
DIMENSIONS

All Variants

Configuration thick cylinder with smaller rounded re-entry

vehicle (RV) on Mod 1, fuller section RV on

Mod 3

Diameter 5 ft 11 in (1.80 m)

Engine single-stage liquid-fuel rocket

Power 50,740 lb (23,000 kg) initial thrust
PERFORMANCE

All Variants

Trajectory altitude 339 nm (390 mi, 628 km) max

CEP 1.0 nm (1.2 mi, 1.9 km)

Launch depth 131-164 ft (40-50 m)

Launch sea state 5 max

Launch latitude up to 85 deg N

Launch sub speed 4 kts max

SS-N-6 Mod 1

Range 1,300 nm (1,497 mi, 2,409 km)

Range 1,600 nm (1,842 mi, 2,965 km)

Warhead 1 x 1 Mt multi-stage thermonuclear device

Warhead 3 x 200 kt nuclear RVs

Guidance inertial