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| R-1 |
 |
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 |
R-1 (8Zh38)
(SS-1A)
Engines:
1. 1 × RD-100
Total mass: 13,248 kg
Ceiling: 85 km
Maximum range: 260
km
Warhead: 547
kg
First launch: 1948 |
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| R-2 |
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|
R-2 (8Zh38)
(SS-2)
Engines:
1. 1 × RD-101
Total mass: 20,091 kg
Apogee: 150
km
Maximum range: 550
km
Warhead: 570 kg
First launch: 1950 |
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| R-5 |
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|
R-5 (8A62)
(SS-3)
Engines:
1. 1 × RD-103
Total mass: 27,250 kg
Apogee: 300
km
Maximum range: 1,190
km
Warhead: 1,375 kg
First launch: 1953 |
|
R-5M (8K51)
Engines:
1. 1 × RD-103M
Total mass: 28,610 kg
Apogee: 500
km
Maximum range: 1,190
km
Warhead: 1,350 kg
First launch: 1955 |
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|
R-7 (8K71)
Engines:
1. 4 × RD-107-8D74-1959
2. 1 × RD-108-8D75-1959
Total mass: 279,100 kg
Apogee: 1,000
km
Maximum Range: 8,000 km
Warhead: 5,370 kg / 3
MT
Accuracy (CEP): 3.39 km
First launch: 1957 |
|
R-7A (8K74)
(SS-6)
Engines:
1. 4 × RD-107-8D74-1959
2. 1 × RD-108-8D75-1959
Total mass: 272,900 kg
Maximum Range: 11,000 km
Warhead: 5,400 kg / 3
MT
First launch: 1959
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| R-7 |
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| R-9 |
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R-9 (8K77,
8K76)
(SS-8)
Engines:
1. 1 × RD-111
2. 1 × RD-0106
Total mass: 80,500
kg
Apogee: 1,000 km
Maximum range: 16,000
km
Warhead: 1,100 kg / 1.65 MT
Accuracy (CEP): 5 km
First launch: 1961 |
|
|
|
 |
Engines:
2. 4 × NK-9
2. 1 × NK-9V
3. 1 × 8D726
Total mass: 117,000
kg
Warhead: 2,300
kg / 2.2 MT
Cancelled: 1964 |
 |
Never flown |
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| R-11 |
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R-11 (8A61)
(SS-1b / Scud A)
Engines:
1. 1 × S2.253
Total mass: 5,337 kg
Apogee: 78 km
Maximum range: 270 km
Warhead: 690
kg
Accuracy (CEP): 1.5
km
First launch: 1954 |
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| R-17 |
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R-17 (9K72)
(SS-1C / Scud B)
Engines:
1. 1 × S5.2
Total mass: 6,350 kg
Maximum range: 300 km
Warhead: 985 kg
Accuracy (CEP): 1.5
km
First launch: 1959 |
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| R-12 |
|
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|
R-12 (8K63)
(SS-4)
Engines:
1. 1 × RD-214
Total mass: 34,914
kg
Apogee: 500 km
Maximum range: 1,500 km
Warhead: 700 kg / 1 MT
Accuracy (CEP): 5.16
km
First launch: 1957
Operational Capability: 1959 |
|
R-12U (8K63U)
Total mass: 41,750
kg
Apogee: 402 km
Maximum range: 2,150 km
Warhead: 1,600 kg / 2.3 MT
Accuracy (CEP): 2.40
km
Operational Capability: 1963 |
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| R-14 |
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R-14 (8K65)
(SS-5)
Engines:
1. 1 × RD-216
Total mass: 86,300 km
Apogee: 500 km
Maximum range: 3,700
km
Warhead: 680 kg / 1
MT
Accuracy (CEP): 1.13 km |
|
R-14U (8K65U
Engines:
1. 1 × RD-216
Total mass: 86,400
kg
Apogee: 676 km
Maximum range: 4,000
km
First launch: 1960
Operational Capability: 1961 |
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| R-16 |
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R-16 (8K64)
(SS-7)
Engines:
1. 1 × RD-218
2. 1 × RD-219
Total mass: 140,600
kg
Apogee: 1,000
km
Maximum range: 13,000
km
Warhead: 1,475 kg / 3 MT
Accuracy (CEP): 2.70
km
First launch: 1960
Operational Capability: 1961
|
|
R-16U (8K64U)
Engines:
1. 1 × RD-218
2. 1 × RD-219
Total mass: 146,600
kg
Apogee: 1,000
km
Maximum range: 13,000
km
First launch: 1961 |
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| UR-200 |
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UR-200B (8K83)
Engines:
1. 1 × RD-0202
2. 1 × RD-0205
Total mass: 135,710
kg
Apogee: 185 km
Maximum range: 12,000
km
Warhead: 2,683 kg / 5 MT
Maximum range: 10,000
km
Warhead: 3,900
kg / 1.5 MT
First launch: 1963 |
|
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|
|
Engines:
1. 4 × RD-0202
2. 4 × RD-0205
3. 1 × RD-0205
Total mass: 571,050
kg
Apogee: 200 km
Warhead: 10,000
kg
Payload:
Design: 1962 |
|
Never flown |
|
| Proton 8K82 |
 |
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| UR-500 (IBCM) |
 |
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UR-500 (8K82)
Engines:
1. 6 × RD-253
2. 4 × RD-0208, RD-0209 Payload (LEO): 8,400 kg
Total mass: 595,490
kg
Apogee: 300 km
Maximum range: 10,000
km
Warhead: 12,200 kg / 100 MT
First launch: 1965
Operational: never deployed |
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| UR-100 |
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UR-100 (15A10) |
|
UR-100K (15A20)
(SS-11) |
| |
Engines:
1. 1 × RD-0216
2. 1 × 15D13
Total mass: 183,890
kg
Apogee: 300 km
Maximum range: 10,000
km
Apogee: 1000
km
Maximum range: 11,000
km
Warhead: 770
kg / 0.5
MT
Accuracy (CEP): 1.40
km
First launch: 1965
Operational Capability: 1966 |
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| R-36 |
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| R-36 Orb |
|
| R-36P |
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R-36 (8K67)
(SS-9)
c
Engines:
1. 1 × RD-251
2. 1 × RD-252
Total mass: 183,890
kg
Apogee: 1,000
km
Maximum range: 10,200
km
Warhead: 5,825
kg / 10
MT
Accuracy (CEP): 1.30
km
First launch: 1963 |
|
R-36 (8K67P)
Engines:
1. 1 × RD-251
2. 1 × RD-252
Total mass: 183,000
kg
Warhead: 5,825 kg / 3 × 2 MT
First launch: 1968 |
|
R-36 orb (8K69)
(SS-X-10)
Engines:
1. 1 × RD-251
2. 1 × RD-252
3. 1 × RD-854
Total mass: 182,000
kg
Apogee: 1,000 km
Warhead: 1,700 kg / 5 MT
Accuracy (CEP): 1.30 km
First launch: 1965 |
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| |
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| R-36M |
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| |
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| R-36M2 |
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R-36M (15A14)
(SS-18)
Engines:
Total mass: 209,600 kg
Maximum range:
11,200
km
9,250
km (MIRV)
Warhead:
7,250 kg
/ 1 × 24.0 MT
/ 8 × 0.50 MT
Accuracy (CEP): 0.43
km
First launch: 1971 |
|
R-36M UTTH (15A18)
Engines:
First launch: 1977 |
|
R-36M2 (15A18M2)
Engines:
Total mass: 211,100 kg
Maximum range:
11,000
km (MIRV)
15,000
km
Warhead: 8,800 kg
/ 1 × 20.0 MT
/ 10 × 0.55 MT
Accuracy (CEP): 0.26
km
First launch: 1986 |
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| UR-100N / NU |
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UR-100N (15A30) |
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UR-100NU (15A35)
(SS-19) |
| |
Engines:
1. 4 × RD-0233
2. 1 × RD-0235
Total mass: 105,600
kg
Maximum range: 10,000
km
Warhead: 4,350 kg
/ 1 × 5.00 MT
/ 6 × 0.55 MT
Accuracy (CEP): 0.31
km
First launch: 1972 |
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| MR-UR-100 |
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MR-UR-100 (15A15) |
|
MR-UR-100U (15A16)
(SS-17) |
| |
Engines:
1. 1 × RD-268
2. 1 × RD-862
Total mass: 71,100 kg
Maximum range: 10
320 km
Warhead:
2 550 kg
/ 1 × 3.6 MT
/ 4 × 0.3 MT
Accuracy (CEP): 0.45
km
First launch: 1971 |
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R-29R (4K75R)
(SS-N-18)
Total mass: 34,388
kg
Maximum range: 6,500
kg
Warhead: 1,300 kg / 3 × 0.2 MT
Accuracy (CEP): 1.40 km
|
|
R-29RM (4K75RM)
(SS-N-23)
Total mass: 40,300
kg
Maximum range: 8,310
km
Wh: 1,810 kg / 10 × 0.1 MT
Accuracy (CEP): 0.9 km |
|
|
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| RT-1 |
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|
RT-1
Engines:
1. 1 × RT-1-1
2. 1 × RT-1-2
3. 1 × RT-1-3
Total mass: 31,900
kg
Maximum range: 2,000 km
Warhead: 800
kg
First launch: 1962 |
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| RT-2 |
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RT-2 (8K98) |
|
RT-2P (8K98P)
(SS-13) |
| |
Engines:
1. 1 × 15D23P
2. 1 × 15D24P
3. 1 × 15D94
Total mass: 51,900
kg
Maximum range: 10,200
km
Warhead: 470 kg / 0.75 MT
Accuracy (CEP): 1.50 km
First launch: 1966 |
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| RT-20 |
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RT-20 (8K99 |
|
RT-20P (8K99P)
(SS-15) |
| |
Engines:
1. 1 × 15D151
2. 1 × RD-857
Apogee: 1,000
km
Maximum range: 7,000
km
Warhead: 545
kg
First launch: 1967 |
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RT-23 (15Zh60)
(SS-24)
Engines:
1.
2.
3.
wh. |
1 × 15D206 (RT23)
1 × 15D305 (RT23U)
1 × 15D339 (RT23U)
1 ×
1 × RD-866 |
Total mass: 104,500
kg
Maximum range: 10,110
km
Warhead: 4,050 kg / 10 × 0.3 MT
First launch: 1982
Operational Capability: 1983 |
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RT-21 (15Zh42)
Temp-2S (SS-16)
Engines:
1. 1 ×
2. 1 ×
3. 1 ×
Total mass: 44,200
kg
Apogee: 1,000 km
Maximum range: 10,500
km
Warhead: 540 kg / 0.65 MT
Accuracy (CEP): 1.64 km
First launch: 1972 |
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RSD-10 Pioner
(15Zh45) (SS-20)
Engines:
1. 1 ×
2. 1 ×
Total mass: 37,000
kg
Apogee: 500 km
Maximum range: 5000
km
Warhead: 1,740 kg
/ 1 × 1.00 MT
/ 3 × 0.15 MT
Accuracy (CEP): 0.55 km
First launch: 1974 |
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| RT-2PM |
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RT-2PM Topol
(15Zh58) (SS-25)
Engines:
1. 1 × 15Zh58A
2. 1 × 15Zh58B
3. 1 × 15Zh58V
Total mass: : 44,200
kg
Apogee: 1,000 km
Maximum range: 10,500
Warhead: 1,810 kg
/ 0.65 MT
Accuracy (CEP): 0.21 km
First launch: 1981 |
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RT-2PM2 Topol-M |
|
(15Zh65) (SS-X-27) |
| |
Total mass:
47,200 kg
Apogee: 1,000 km
Maximum range: 10,500
km
Warhead: 1.2
t / 1.00 MT
Accuracy (CEP): 0.21 km |
|
RS-24 YaRS
(SS-X-29)
First launch: 1994 |
|
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RS-26 Rubezh
(SS-X-31)
Engines:
1. 1 × 15Zh58MA
2. 1 × 15Zh58MB
Total mass: 36,00 kg
Maximum range: 5800
km
Warhead: 0.8
t / 4 × 0.15 - 0.3 MT
Accuracy (CEP): 0.09 - 0.21 km
First launch: 2011
| |
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R-30 Bulava
(SS-NX-30)
Total mass: :
47,200 kg
Apogee: 1,000 km
Maximum range: 10,500
km
Warhead: 9-10 × 0.1-0.5 MT
First launch: 2005 |
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Tochka (9K79)
(SS-21)
Total mass: 2,010 kg
Maximum range: 138 km
Warhead: 680 kg
First launch: 1975
Operational Capability: 1976 |
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|
Iskander (9M723)
(SS-26)
Total mass: 3,800 kg
Maximum range: 400-500 km
Warhead: 480-700 kg
Operational Capability: 2006 |
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