Andegraf Rockets
 1   2   3   4   5   6   7   8   9   10   11   12 
 
 

 
   
R1 (8Zh38) (SS-1A)
   
Engines:
1. 1 × RD-100
   
Total mass: 13,248
Ceiling: 85 km
Maximum range: 260 km
Warhead: 547 kg 

First Launch: 1948

 
   
R2 (8Zh38) (SS-2)
   
Engines:
1. 1 × RD-101
   
Total mass: 20,091
Apogee: 150 km
Maximum range: 550 km
Warhead: 570 kg

First Launch: 1950
 
     
R5 (8A62) (SS-3)
   
Engines:
1. 1 × RD-103
   
Total mass: 27,250
Apogee: 300 km
Maximum range: 1,190 km
Warhead: 1,375 kg 

 
   
R5M (8K51) (SS-3)

   
Engines:
1. 1 × RD-103M
   
Total mass: 28,610
Apogee: 500 km
Maximum range: 1,190 km
Warhead: 1,350 kg 
 
First Launch: 1953
     
R7 (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)
Warhead CEP: 3,39 km

 
   
R7A (8K74)
(SS-6)
   
Engines:
1. 4 × RD-107-8D74-1959
2. 1 × RD-108-8D75-1959
   
Total mass: 272,900 kg
Apogee: 1,000 km
Maximum Range: 11,000 km
Warhead: 5,400 kg (3 MT)
Warhead CEP: 3,39 km

First Launch: 1957
  
Launches >>
     
R9 (8K77, 8K76, 8K75)
(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)
Warhead CEP: 5 km

First Launch: 1961
     
GR-1 (8K713)
   
Engines:
1. 4 × NK-9
2. 1 × NK-9V
3. 1 × 8D726
   
Warhead: 2,300 kg (2,2 MT)
Total mass: 117,000 kg 

Cancelled: 1964
     
R11 (8A61, 8K11, 8K12)
(SS-1b / Scud A)

   
Engines:
1. 1 × S2.253
   
Total mass: 5,337 kg
Apogee: 78 km
Maximum range: 270 km
Warhead: 690 kg 
Warhead CEP: 1,5 km

First Launch: 1954
     
R17 (9K72)
(SS-1C / Scud B)
   
Engines:
1. 1 × Isayev R-17
   
Total mass: 6,350 kg
Maximum range: 300 km
Warhead: 985 kg 
Warhead CEP: 1,5 km

First Launch: 1959
 
   
R12 (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)
Warhead CEP: 5,16 km

First Launch: 1957
Operational Capability: 1959

 
   
R12U (8K63U)
(SS-4)
   
Engines:
1. 1 × RD-214
   
Total mass: 41,750 kg 
Apogee: 402 km
Maximum range: 2,150 km
Warhead: 1,600 kg (2,3 MT)
Warhead CEP: 2,40 km

Operational Capability: 1959
     
R14 (8K65) (SS-5)
   
Engines:
1 × RD-216
   
Total mass: 86,300
   
Apogee: 500 km
Maximum range: 3,700 km
Warhead: 680 kg (1 MT)
Warhead CEP: 1,13 km

 
   
R14U (8K65U)
(SS-5)
   
Engines:
1. 1 × RD-214
   
Total mass: 86,400 kg
Apogee: 676 km
Maximum range: 4,000 km

First Launch: 1960
Operational Capability: 1961
     
R16 (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)
Warhead CEP: 2,70 km

 
   
R16U (8K64U)
(SS-7)
   
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: 1960
Operational Capability: 1961
     
UR200 (8K81) (SS-10)
   
Engines:
1. 1 × RD-0202
2. 1 × RD-0205

 
   
UR200B (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
     
UR500 (8K82)
   
Engines:
1. 6 × RD-253
2. 3 × RD-02081 × 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
     
UR-100N
UR-100NU 
 
(15A30)
(15A35) 
(SS-19)
   
Engines:
1. 1 × RD-0216
2. 1 × 8D423
   
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)
Warhead CEP: 1,40 km

First Launch: 1965
 
   
R36 (8K67) (SS-9)
   
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)
Warhead CEP: 1,30 km

 
   
R36 (8K67P)
(SS-9)
   
Engines:
1. 1 × RD-251
2. 1 × RD-252
   
Total mass: 183,000 kg 
Warhead: 5,825 kg  (3 × 2 MT)

First Launch: 1963
 
   
R36 orb (8K69)
(SS-X-10)

   
Engines:
1. 1 × RD-251
2. 
1 × RD-252
31 × RD-854
   
Total mass: 182,000 kg 
Apogee: 1,000 km
Maximum range: 10,200 km
Warhead: 1,700 kg (? MT)
Warhead CEP: 1,30 km

First Launch: 1965
 
   
R-36M (15A14) (SS-18)
   
Engines:
1. 
2. 
1 × RD-264
1 × RD-0228
wh  ? × RD-?
   
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)
   
Warhead CEP: 0,43 km

First Launch: 1971
 
   
R-36M UTTH (15A18)
   
Engines:
1. 
2. 
1 × RD-264
1 × RD-0255
wh  4 × RD-869

First Launch: 1977






 
   
R-36M2 (15A18M)

   
Engines:
1.
2. 
1 × RD-264
1 × RD-0255
wh  4 × RD-869
   
Total mass: 211,100 kg
   
Maximum range:
11,000 km (MIRV)
15,000 km
   
Warhead:
8,800 kg   (10 × 0,55 MT)
(8 × 20,0 MT)
 
   
Warhead CEP: 0,26 km

First Launch: 1986
     
UR-100N
UR-100NU 
(15A30)
(15A35) 
(SS-19)
   
Engines:
1. 4 × RD-0232
2. 1 × RD-0235
   
Total mass: 105,600 kg
   
Maximum range: 10,000 km
   
Warhead:
4,350 kg   (1 × 5,0 MT)
(6 × 0,55 MT)
   
Warhead CEP: 0,31 km

First Launch: 1972
     
MR-UR-100
MR-UR-100U  
(SS-17)
(15A15
(15A16)
  
Engines:
1. 1 × RD-268
2. 1 × RD-862
   
Total mass: 71,100 kg 
   
Maximum range: 10 320 km
   
Warhead:
2 550 kg  (4 × 0,3 MT)
(1 × 3,6 MT)
   
Warhead CEP: 0,45 km

First Launch: 1971
     
R29 (4K75) (SS-N-5)
 
R29R (4K75R) (SS-N-185)
   
Total mass: 34,388 kg 
Warhead: 1,300 kg (3 0,2 MT)
Maximum range: 6,500 km
Warhead CEP: 1,40 km
 
R29RM (4K75RM)
(SS-N-23)

   
Total mass: 40,300 kg
Maximum range: 8,310 km
Warhead: 1,810 kg (10 × 0,1 MT) 
Warhead CEP: 0,9 km
     
RT-1
   
Engines:
1. 
1 × RT-1-1
2. 1 × RT-1-2
31 × RT-1-3
   
Total mass: 31,900 kg 
Maximum range: 2,000 km
Warhead: 800 kg

First Launch: 1962
     
RT-2
RT-2P 
(8K98)
(8K98P)
(SS-13)
   
Engines:
1. 
1 × 15D23P
2. 1 × 15D24P
31 × 15D94
   
Total mass: 51,900 kg 
Maximum range: 10,200 km
Warhead: 470 kg (0,75 MT)
Warhead CEP: 1,50 km

First Launch: 1966
     
RT-20
RT-20P 
(8K99)
(8K99
P
(SS-15)
   
Engines:
1. 
1 × 15D151
2. 1 × RD-857
   
Apogee: 1,000 km
Maximum range: 7,000 km
Warhead: 545 kg (? MT)
Warhead CEP: ? km

First Launch: 1967
     
RT-23 (15Zh60)
(SS-24)

   
Engines:
1. 
1 × 15D206 (RT23)
    1 × 15D305 (RT23U)
2. 1 × 15D339 (RT23U)
3. 1 × ?
   
Total mass: 104,500 kg 
Maximum range: 10,110 km
Warhead:4,050 kg (10 x 0,3 MT)

First Launch: 1982
Operational Capability: 1983
     
RT-21Temp-2S (15Zh42)
(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)
Warhead CEP: 1,64 km

First Launch: 1972
     
RSD-10 Pioner (15Zh45)
(SS-20)

   
Engines:
1. 
1 × ?
2. 1 × ?
   
Total mass: 37,000 kg 
Apogee: 500
Maximum range: 5000 km
   
Warhead:
1,740 kg   (3 × 0,15 MT)
(1 1,00 MT)
   
Warhead CEP: 0,55 km

First Launch: 1974
     
RT-2PM Topol (15Zh58)
(SS-25)

   
Engines:
1. 
1 × 15Zh58A
2. 1 × 15Zh58B
3. 1 × 15Zh58B
4. 1 × 15Zh58V
   
Total mass: : 44,200 kg 
Apogee: 1,000 km
Maximum range: 10,500
   
Warhead:
1,810 kg (0,65 MT)
   
Warhead CEP: 0,21 km

First Launch: 1981
     
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)
Warhead CEP: 0,21 km

   
RT-2M2 YaRS (?)
(SS
-X-29)


First Launch: 1994
     
R30 Bulava
   
Total mass: : 47,200 kg
Apogee: 1,000 km
Maximum range: 10,500 km
Warhead: ( 10 x ? MT)

First Launch: 2005
     
Iskander (9M723)
(SS-26)
   
   
Total mass: 3,800 kg
Maximum range: 400-500 km
Warhead: (480-700 kg)

Operational Capability: 2006
 
 1   2   3   4   5   6   7   8   9   10   11   12