Titan SMw68
SPECIFICATIONS
Length: 98 ft
Weight: 220,000 lb
Diameter: First stage - 1 0 ft
Second stage-8 ft
PERFORMANCE
Speed: 15,000 mph
Apogee: 500 mi
Range: 5500 to 6300 mi
CEP: about a half mile
PROPULSION: Liquid fuel rocket engines burning liquid
oxygen and RP-1 (alcohol).
First stage: Two Aerojet LR-87-AJ-1
Max thrust: 300,000 lb
Second stage: Single Aerojet LR-91-AJ-1
Max thrust: 80,000 lb
GUIDANCE
Radio Command guidance system developed
by
Bell Telephone Lab and Remington Rand
UNIVAC
WARHEAD
Either a single W-38, or a W-49 thermonuclear
warhead of four megaton yield in a
Mk-4 re-entry
vehicle
CONTRACTOR
Glen L Martin Company (Now Martin
Marietta)
NUMBER OF MISSILES DEPLOYED
54 deployed; 163 constructed, 67 flown