Jump to content

Mayak (rocket family)

From Wikipedia, the free encyclopedia

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

[edit]
  1. ^ "Mayak". State Space Agency of Ukraine. Retrieved 7 November 2015.
  2. ^ a b "Launch vehicles / Missiles / Mayak". Design Office. Retrieved May 25, 2016.