USSR / Russia
1 2 3 4 5 6 7 8 9 10 11 12
Strela
UR-100N (15A30)

UR-100NU  (15A30)
 
Engines:
1.4 ×RD-0233
2.1 ×RD-0235

Total mass: 105,600 kg
Apogee: 1,000 km
Maximum range: 9,650 km
Warhead: 4,350 kg


Strela

Engines:
1.4 ×RD-0233
2.1 ×RD-0235
3.1 ×Post boost Module

Total mass: 104,000 kg
Apogee: 200 km
Payload weight:
(LEO) 1,700 kg(200 km, 74)
(SSO) 1,100 kg


Rokot

Engines:
1.
2.
4 ×RD-0233
1 ×RD-0235
3. 1 ×S5.98M | Briz-K
1 ×S5.98M | Briz-KM
1 ×S5.98M | Briz-KS
(K)
(KM)
(KS)

Total mass: 107,000 kg
Apogee: 200 km

Payload weight:
(LEO) 1,850 kg
1,950 kg
(K)
(KM)
(LPEO)
(SSO)
2,000 kg
1,200 kg
(KS)
(KM)

Launches: 38 (Failures: 3)
/1990-2019/
L F
(Strela)
3   /2003-2014/
(Rokot)
K
KM
4
31
1
2
/1990-1999/
/2000-2019/
Payload:

(Strela) , , -

(Rokot K) -, , -

(Rokot KM) SimSat, GRACE, Iridium, MOST, MIMOSA, CanX, AAU-Cubesat, DTUSat, QuakeSat, ×I-IV, CUT, SERVIS, -E, CryoSat, KOMPSat, -3, , GOCE, SMOS, PROBA, -M, --2, Swarm, , Sentinel
Rokot K
Rokot KM
 
Dnepr

R-36M2 (15A18M)

Engines:
1.
2.
1 ×RD-264
1 ×RD-0255
wh 4 ×RD-869

Total mass: 211,100 kg
Maximum range: 15,000 km
Warhead: 8,800 kg


Dnepr

Engines:
1.1 ×RD-264
2.1 ×RD-0255
3.4 ×RD-869

Total mass: 208,900 kg

Payload weight:
(LEO)
(LPEO)
(IPT)
3,700 kg
2,650 kg
700 kg

Launches:21 (Failures: 1)
/1999-2015/
Payload: UoSat, MegSat, Unisat, SaudiSat, Tiungsat, Rubin, LatinSat, TrailBlazer, DEMETER, OICETS, INDEX, Genesis, , , PicPot, CP, HAUSAT, ICECube1, ION, KUTESat-Pathfinder, MEROPE, Ncube, Rincon, SACRED, SEEDS, AeroCube, EgyptSat, SaudiComsat, MAST, CAPE, CSTB, Libertad, TerraSAR-X, RapidEye, THEOS, DubaiSat, Deimos, CryoSat, Picard, PRISMA Main, PRISMA Target, BPA, TanDEM-X, , NigeriaSat, NX, RASAT, EDUSAT, AprizeSat, KOMPSat, STSAT, SkySat, WNISAT, BRITE-PL, AprizeSat, Delfi-n3Xt, Dove, Triton, CINEMA, OPTOS, CubeBug, GOMX, NEE, Krysaor, FUNcube, HiNCube, ZACUBE, ICube, HumSat-D, PUCP-SAT, First-MOVE, UWE, VEO, BeakerSat, $50SAT, QubeScout, S1, Wren, Pocket-PUCP, BPA, KazEOSat, Hodoyoshi, TabletSat-Aurora , BugSat, Perseus, POPSAT-HIP, TigriSat, Lemu, ANTELSAT, QB50P, QB50P2, PACE, Duchifat, NanoSatC-Br, PolyITAN, DTUSat, ASNARO, ChubuSat, QSAT-EOS, Tsubame, KOMPSAT...
   
Volna
Volna 0
Shtil
R-29 (4K75)


 
R-29R (4K75R)

Total mass: 34,388 kg
Warhead: 1,300 kg / 3 ×0.2 MT
Maximum range: 6,500 km
Accuracy (CEP): 1.40 km



Volna

Engines:
1.1 ×RD-0244
2.1 × 3D41
3.1 ×?

Payload weight:
(LEO) 115 kg



Shtil

Engines:
1.1 ×RD-0244
2.1 × 3D41
3.1 ×?

Payload weight:
(LEO) 280 kg
200 kg
220 kg
(Shttil 1)
(Shttil 2.1)
(Shttil 2R)

Launches: 7 (Failures: 3)
/1995-2006/
L F
(Volna)
(Volna O)
(Shtil)
4
1
2
2
1
/1995-2005/
/2005-2005/
/1998-2006/
Payload: CM, Tubsat, IRDT (Inflatable Re-Entry and Descent Technology), Cosmos, Kompas
Start
Start 1
Start 1.2
RT-2PM Topol (15Zh58)

Total mass: : 44,200 kg
Apogee: 1,000 km
Warhead:1,000 kg
Maximum range: 10,500 km


Start

Engines:

Engines:
1.
1 ×15Zh58A
2.1 ×15Zh58B
3.1 ×15Zh58B
4.1 ×15Zh58V

5.1 ×Start

Total mass: 60,000 kg
Apogee: 200 km

Payload weight:
(LEO) 645 kg(300 km, 30)
570 kg(400 km, 30)



Start-1

Engines:
1.1 ×15Zh58A
2.1 ×15Zh58B
3.1 ×15Zh58V

4.1 ×Start

Total mass: 47,200 kg
Apogee: 200 km

Payload weight:
(LEO)632 kg(200 km, 52)

Launches: 7 (Failures: 1)
/1993-2006/
L F
(Start)
(Start-1)
(Start-1.2)
1
5
1
1 /1995-1995/
/1993-2006/
/1997-1997/
Payload: EKA, Techsat, , EROS, Odin, Earlybird
Missiles SuborbitalR-7 (Soyuz)Ur-500 (Proton)R-12, R-14 (Kosmos)
R-36 (Tsiklon)ICBM DerivativesN1EnergiaZenitAngaraUnflown