Reliability improvements included all-electric design (hydraulic power for control surfaces was eliminated) and solid-state electronics with the first battery power in a US Missile. These improvements reduced the warm-up time from 27 seconds down to 1/15 of a second. RIM-66A was an interim missile that used the existing Tartar Mark 27 motor. RIM-66B introduced a new dual-thrust motor to achieve greater speed and range. The SM-1 MR, SM-2 MR and Tartar missiles are virtually identical in appearance but quite different in performance. |
![]() Standard Missile 1 MR RIM-66B
|
Designation | Standard MR RIM-66A and RIM-66B |
Ship Class Used On | Many |
Date In Service | Block III: 1967
Block IV: 1970 |
Weight | 66A: 1,240 lbs. (562 kg)
66B: 1,390 lbs. (630 kg) |
Dimensions | 13.5 x 176 in (34 x 447 cm)
Span 42.5 in (108 cm) |
Payload | 137 lbs. (62 kg) continuous rod |
Range | 66A: 3,000 - 35,000 yards (2,750
- 32,000 m)
65,000 feet (19,800 m) max altitude 66B: 3,000 - 50,000 yards (2,750
- 45,700 m)
|
Propulsion | Boost-sustainer rocket |