 |
|
|
|
|
UR-100N
UR-100NU |
(15A30)
(15A35) |
(SS-19) |
Engines:
1. 4 × RD-0233
2. 1 × RD-0235
Total mass: 105,600
kg
Apogee: 1,000
km
| Warhead: |
4,500 kg
(6 × 0,55 MT)
(1 × 5 MT) |
Maximum range: 9,650
km
CEP: 0,26 km
|
|
| |
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:
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: |
| (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
Rokot KM
Rokot KS |
4
31 |
1
2 |
/1990-1999/
/2000-2019/ |
| |
|
Payload:
(Strela) Грузомакет, Кондор, Кондор-Е
(Rokot K) Наряд-В, Можаец, Радио-РОСТО
(Rokot K) SimSat, GRACE, Iridium, MOST, MIMOSA, CanX, AAU-Cubesat, DTUSat, QuakeSat, XI-IV, CUT, SERVIS, Монитор-E, CryoSat, KOMPSat, Стрела-3, Юбилейний, GOCE, SMOS, PROBA, Гонец-M, Гео-ИК-2, Swarm, Космос, Sentinel
|
|
|
|
|
|
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 |
Dnepr
Engines:
1. 1 × RD-264
2. 1 × RD-0255
3. 4 × RD-869
Total mass: 208,900 kg
| Payload: |
(LEO)
(LPEO)
(DSO)
(IpT) |
3,700 kg
2,650 kg
500 kg
700 kg |
Launches:21 (Failures: 1)
/1999 - 2015/
| |
L |
F |
|
Dnepr
Dnepr M |
22 |
1 |
/1999 - 2015/ |
| |
|
|
|
| Dnepr (SBS) |
SBS 1
SBS 2
SBS 3 |
|
|
|
|
Payload: UoSat, MegSat, Unisat, SaudiSat, Tiungsat, Rubin, LatinSat, TrailBlazer, DEMETER, OICETS, INDEX, Genesis, БелКа, Бауманец, 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, Сич, 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, VELOX, 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...
|
|
|
|
|
|
R29 (4K75)
(SS-N-5)
R29R (4K75R)
(SS-N-185)
Total mass: 31,300
kg
| Warhead: |
4,500 kg (3 x 0.2 MT) |
Maximum range: 6,500
km
Warhead CEP: 1,40
Volna
Engines:
1. 1 × RD-0243
2. 1 × ?
3. 1 × ?
Shtil
Engines:
1. 1 × RD-0243
2. 1 × ?
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 |
4 |
2 |
/1995-2005/ |
| Volna O |
1 |
1 |
/2005-2005/ |
| |
|
|
|
| Shtil |
2 |
|
/1998-2006/ |
| Shtil 2.1 |
|
|
|
| Shtil 2R |
|
|
|
|
|
Payload: CM, Tubsat, IRDT (Inflatable Re-Entry and Descent Technology), Cosmos, Kompas |
|
|
|
|
RT-2PM Topol (15Zh58)
(SS-25)
Total mass: : 44,200
kg
Apogee: 1,000
km
| Warhead: |
1,000 kg |
| |
(0,65 MT) |
Maximum range: 10,500 km
Apogee: 1,000 km
Warhead CEP: 0,21 km
Start
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) |
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) |
Launches: 7 (Failures: 1)
/1993-2006/
| |
L |
F |
|
| Start |
1 |
1 |
/1995-1995/ |
| Start 1 |
5 |
|
/1993-2006/ |
| Start 1.2 |
1 |
|
/1997-1997/ |
|
Payload: EKA, Techsat, Можаец, EROS, Odin, Earlybird, EROS, Odin |
|
|
|
