SLAM Supersonic Low-Altitude Missile
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English |
Metric |
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Characteristics |
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Diameter (ft/cm) |
5 |
152 |
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Length (ft/cm) |
65 |
1981 |
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Gross Weight (lb/kg) |
45000 |
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Range |
Essentialy |
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Speed (Mach) |
3 |
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(Speed is the same as a rifle bullet 2280 mph) |
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Payload |
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16 one-megaton bombs |
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Propulsion |
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600 Megawatts from nuclear reactor |
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(Power is one-half the power output of Boulder Dam) |
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Guidance Systems |
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Inertial plus TERCOM |
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(TERCOM was developed for this program) |
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Other Facts |
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Lift/Drag Ratio - 2/1 |
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Missile Skin Temp - 1,000 degrees Fahrenheit |
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Airframe Material - Rene 41 Stainless Steel - Gold plated for radiation cooling |
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Skin Thickness - 1/10 to 1/4 inch |
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Flight Profile - Launch from mobile or stationary launchers from any point on earth by 3 solid propellant booster rockets to a high-altitude cruise, then decend to altitudes of 100 ft or so for Mach 3 penetration to the target area on any other part of the earth and eject 16 one-megaton hydrogen bombs to separate targets. |
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