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| UR-100N / NU |
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| Strela |
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| |
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| Rokot K |
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| Rokot KM |
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UR-100N (15A30) |
|
UR-100NU (15A35) |
| |
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: |
| (LEO) |
1,700
kg (200 km, 74 ) |
| (SSO) |
1,100 kg |
|
|
Rokot
Engines:
Total mass: 107,000 kg
Apogee: 200
km
Payload:
| (LEO) |
1,850 kg
1,950 kg |
(K)
(KM) |
| |
|
|
(LPEO)
(SSO) |
2,000 kg
1,200 kg |
(KS)
(KM) |
|
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Launches: 38 (Failures: 3)
/1990-2019/
| |
L |
F |
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| (Strela) |
| · |
3 |
|
/2003-2014/ |
| |
| (Rokot) |
· K
· KM |
4
31 |
1
2 |
/1990-1999/
/2000-2019/ |
Payload:
(Strela) Ãðóçîìàêåò, Êîíäîð, Êîíäîð-Å
(Rokot K) Íàðÿä-Â, Ìîæàåö, Ðàäèî-ÐÎÑÒÎ
(Rokot KM) SimSat, GRACE, Iridium, MOST, MIMOSA, CanX, AAU-Cubesat, DTUSat, QuakeSat, × I-IV, CUT, SERVIS, Ìîíèòîð-E, CryoSat, KOMPSat, Ñòðåëà-3, Þáèëåéíèé, GOCE, SMOS, PROBA, Ãîíåö-M, Ãåî-ÈÊ-2, Swarm, Êîñìîñ, Sentinel |
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| R-36M2 |
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| Dnepr |
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R-36M2 (15A18M)
Engines:
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:
(LEO)
(LPEO)
(IPT) |
3,700 kg
2,650 kg
700 kg |
|
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Launches:21 (Failures: 1)
/1999-2015/
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Payload: UoSat, MegSat, Unisat, SaudiSat, Tiungsat, Rubin, LatinSat, TrailBlazer, DEMETER, OICETS, INDEX, Genesis, ÁåëÊà, Áàóìàíåö, 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, Ñè÷, 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... |
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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 (LEO): 115 kg
|
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Shtil
Engines:
1. 1 × RD-0244
2. 1 × 3D41
3. 1 × ?
Payload (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/ |
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Payload: CM, Tubsat, IRDT (Inflatable Re-Entry and Descent Technology), Cosmos, Kompas |
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| Start |
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RT-2PM Topol
Total mass: : 44,200
kg
Apogee: 1,000
km
Warhead: 1,000 kg
Maximum range: 10,500 km |
|
Start-1
Engines:
1. 1 × 15Zh58A
2. 1 × 15Zh58B
3. 1 × 15Zh58V
4. 1 × Start
Total mass: 47,200 kg
Apogee: 200
km
Payload (LEO):
632 kg (200 km, 52) |
|
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 (LEO):
645 kg (300 km, 30)
570 kg (400 km, 30) |
|
Launches: 7 (Failures: 1)
/1993-2006/
| |
L |
F |
|
(Start)
(Start-1)
(Start-1.2) |
1
5
1 |
1 |
/1995-1995/
/1993-2006/
/1997-1997/ |
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Payload: EKA, Techsat, Ìîæàåö, EROS, Odin, Earlybird |
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