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| Redstone |
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Redstone (PGM-11)
Engines:
1. 1 × A-6
Total mass: 27,800
kg
Maximum range: 325 km
Ceiling: 92 km
Warhead: 3,580 kg / 4 MT
First launch: 1953
Operational Capability: 1958 |
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| Jupter |
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Jupter (PGM-19)
Engines:
1. 1 × S-3D
Total mass: 54,400 kg
Maximum range: 2,980 km
Ceiling: 610
km
Warhead: 1,000 kg / 1.45
M
First launch: 1957
Operational Capability: 1960
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| Thor |
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Thor DM-18 (SM-75)
Engines:
1. 1 × MB-3-1
Total mass: 49,800 kg
Maximum range: 2,400 km
Ceiling: 480 km
Warhead: 1,000 kg / 1.45 MT
First launch: 1957
Operational Capability: 1957 |
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Launches >>
/1957-1962/ |
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| Atlas D |
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| Atlas E / F |
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Atlas D (SM-65A)
Engines:
Total mass: 119,000 kg
Maximum range: 12,100 km
Ceiling: 1,288 km
Warhead:
1,680 kg / 1.44 MT (Mk 2)
1,100 kg / 1.44 MT (Mk 3)
Accuracy (CEP): 3.23 km
First launch: 1959
Operational Capability: 1959
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Atlas E / F (SM-65E/F)
Engines:
Total mass: 121,000 kg
Maximum range: 12,100 km
Ceiling: 1,288 km
Warhead: 1,840 kg
/ 3.75 MT (Mk 4)
Accuracy (CEP): 3.23 km
First launch: 1960 / 1961
Operational Capability: 1960
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| Titan 1 |
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Titan 1 (SM-68)
Engines:
1. 2 × LR-87-3
2. 1 × LR-91-3
Total mass: 105,142 kg
Maximum range: 11,300 km
Ceiling: 1,000 km
Warhead: 1.44
MT
Accuracy (CEP): 2.02 km
First launch: 1959
Operational Capability: 1962 |
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| Titan 2 |
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Titan 2 (SM-68B)
Engines:
1. 2 × LR-87-5
2. 1 × LR-91-5
Total mass: 154,000 kg
Maximum range: 11,690 km
Ceiling: 185
km
Warhead: 3,100 kg / 8.9 MT
Accuracy (CEP): 1.61 km
First launch: 1962
Operational Capability: 1963 |
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Launches >>
/1962-1976/ |
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Minuteman (SM-80)
Engines:
1. 1 × M-55E1
2. 1 × M-56A1
1 × SR-19-AJ-1
3. 1 × M-57A1
1 × SR-73-AJ-1 |
(1, 2, 3)
(1)
(2, 3)
(1, 2)
(3) |
Total mass:
29,400 kg-35,300 kg
Warhead:
450 kg
500 kg
680 kg
1,000 kg
1,000 kg
1,000 kg |
/ 1 × 1.0 MT
/ 1 × 0.8 MT
/ 1 × 1.2 MT
/ 1 × 1.2 MT
/ 1 × 2.0 MT
/ 3 × 0.3 MT |
(1A)
(1B)
(2)
(3)
(3)
(3) |
Maximum range: 13,000 km
Operational Capability: 1962 |
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MX (LGM-118)
Engines:
1. 1 × TU-903
2. 1 × SR-119
3. 1 × SR-120
4. 1 × PBM
Total mass: 88,300 kg
Maximum range: 10,900 km
Ceiling: 1,000 km
Warhead: 3,600 kg / 10 × 0.3 MT
Accuracy (CEP): 0.12 km
Operational Capability: 1986 |
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Pershing 1 (MGM-31)
Engines:
1. 1 × TX-174
2. 1 × TX-175 |
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Pershing 2 (MGM-31C)
Engines:
1. 1 × Hercules
2. 1 × Hercules |
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Polaris A1, A2, A3 (UGM-27)
Total mass:
12,700 kg (A1), 16,200 kg (A3)
Maximum range:
1,900 km (A1), 4,600 km (A3)
Warhead:
500 kg
500 kg
760 kg |
/ 1 × 0,6 MT
/ 1 × 0.6 MT
/ 3 × 0.2 MT |
(A1)
(A2)
(A3) |
Operational Capability: 1961 |
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Poseidon C3 (UGM-73)
Total mass: 29,475 kg
Maximum range: 4,650 km
Warhead: 1,630 kg
/ 10 × 0,05 MT
Accuracy (CEP): 0.53 km
Operational Capability: 1961 |
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Trident I C4 (UGM-96)
Total mass: 33,000 kg
Maximum range: 7,400 km
Warhead: 1,317 kg / 8 × 0.1 MT
Accuracy (CEP): 0.40 km |
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Trident II D5 (UGM-133)
Total mass: 58,900 kg
Maximum range: 11,100 km
Warhead: 1,690 kg
/ 8 × 0.45 MT
Accuracy (CEP): 0.40 km
Operational Capability: 1977
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