Mayak is a new family of Ukrainian launch vehicles under development by the Pivdenne,[1][2] which would be manufactured by Pivdenmash.
The family is built in a modular fashion on the basis of a single line of main engines with thrust of roughly 120 or 200 tonnes-force (1,200 or 2,000 kN) for the first stage (RD-801 or RD-810) and 10 tonnes-force (98 kN) for the upper stage (RD-809K derived from RD-8). Engines, control systems and ground equipment are largely derived from components of existing rocket families Zenit and Tsyklon.
The Mayak family is designed to cover small-lift, medium-lift and heavy-lift requirements. Published parameters of various configurations are:[2]
Version | Mayak-L1 | Mayak-L2 | Mayak-M1 | Mayak-M2 | Mayak-H3 | Mayak-H5 |
---|---|---|---|---|---|---|
Length (m) | 27.3 | 36.9 | 47.4 | 61.0 | 63.0 | 64.0 |
Diameter (m) | 2.7 | 3.0 | 3.9 | |||
Launch mass (t) | 95 | 165 | 370 | 495 / 515 | 1218 / 1236 | 2010 / 2015 |
Number of stages | 2 | 2 / 3 | ||||
Stage 1 engines | 1 × RD-801 | 2 × RD-801 | 2 × RD-810 | 4 × RD-810 | 12 × RD-810 | 20 × RD-810 |
Stage 2 engines | 1 × RD-809K | 2 × RD-809K | 4 × RD-809K | 1 × RD-801B | ||
Optional stage 3 booster | — | RD-809K | ||||
Propellants | LOX / kerosene | |||||
Payload to LEO (t) | 1.5 | 3 | 8.2 | 15.1 / – | 45.5 / – | 70.1 / – |
Payload to GTO (t) | – | – | 2.4 | – / 6.5 | 16 / 19 | 25 / 30.2 |
References
- ↑ "Mayak". State Space Agency of Ukraine. Retrieved 7 November 2015.
- 1 2 "Launch vehicles / Missiles / Mayak". Design Office. Retrieved May 25, 2016.
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