The Mayak launch vehicle family provides spacecraft launches into low and medium orbits, including sun-synchronous.
The launch vehicles use environmentally friendly propellants: liquid oxygen and kerosene.
The Mayak family is derived from the existing Zenit and Cyclone launch vehicles.
The family includes lightweight (Mayak-L1, Mayak-L2), medium-lift (Mayak-M1, Mayak-M2) and heavy-lift (Mayak-H3, Mayak-H5) launch vehicles.
Basic Specifications
|
Mayak-L1 |
Mayak-L2 |
Mayak-M1 |
|
|
Number of stages |
2 |
2 |
2 |
|
Dimensions, mm Length Stage diameter Fairing diameter |
27300 2700 2400 |
36900 3000 4000 |
47400 3900 4000 |
|
Launch mass, tons |
95 |
165 |
370 |
|
Propellants |
liquid oxygen + kerosene |
||
|
Propulsion: Stage 1 Stage 2 Stage 3/Booster stage |
RD801 RD809К - |
2*RD801 2*RD809К - |
2*RD810 4*RD809К - |
|
Thrust, ton-force Stage 1 (sea-level) Stage 2 (vacuum) Booster stage (vacuum) |
123 10 - |
246 20 - |
388 40 - |
|
Maximum payload capability, tons Circular orbit (Hc=200 km, i=51.6°) Geostationary transfer orbit (Hp/Ha =183/35786 km, i=2.3°) |
1500 |
3000 |
8200
2400 |
Basic Specifications
|
Mayak-M2 |
Mayak-H3 |
Mayak-H5 |
|
|
Number of stages |
2/3 |
2/3 |
2/3 |
|
Dimensions, mm Length Stage diameter Fairing diameter |
61000 3900 4600 |
63000 3900 4600 |
64000 3900 6000 |
|
Launch mass, tons |
495/515 |
1218/1236 |
2010/2015 |
|
Propellants |
liquid oxygen + kerosene |
||
|
Propulsion: Stage 1 Stage 2 Stage 3/Booster stage |
4*RD810 RD801В -/RD809К |
12*RD810 RD801В -/RD809К |
20*RD810 RD801В -/RD809К |
|
Thrust, ton-force Stage 1 (sea-level) Stage 2 (vacuum) Booster stage (vacuum) |
776 141,7 - / 10 |
2328 141,7 - / 10 |
3880 141,7 - / 10 |
|
Maximum payload capability, tons Circular orbit (Hc=200 km, i=51.6°) Geostationary transfer orbit (Hp/Ha =183/35786 km, i=2.3°) |
15100/ -
-/ 6500 |
45500/ -
16000/ 19000 |
70100/ -
25000/ 30200 |
Payload Accommodation Area
Lightweight Mayak
Lightweight and Medium-Lift Mayak
Medium- and Heavy-Lift Mayak with Booster Stage
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